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Monday, May 31, 2010

River Rafting / Whitewater Rafting





The challenge of a turbulent river is no less than that of the rugged mountains. The icy heights of the Himalayas are the source of some of India's mighty rivers. Fed by innumerable streams they race along tortuous boulder strewn beds, cutting deep gorges and breaking into silvery white rapids. The term 'White water' refers to foamy and whitish appearance of fast flowing water. The white water river rafting is quite thrilling and adventurous. With the intricate network of mountain rivers flowing through a myriad of different colors of rocky Gorges, forests, flowers and high mountain villages, the hills provide ideal locals for the perfect water adventure

The magic behind River Rafting also referred, as Whitewater River Rafting is the extreme and never-ending thrills in the untamed rivers. The rivers in the upper Himalayas are among the best in the world for river rafting sports, with many staircase rapids that challenge the body and spirit of the river runner. The river cuts against the rocky banks, crash into rocks, crevices and breaking into white water rapids, foaming, swirling, and falling in a thunderous din. India and Nepal has a wide range of river rafting regions, which suits both amateurs and professionals.

Monday, May 24, 2010

General Motors: Weight Loss Diet Program



The following diet and health program was developed for employees and dependents of General Motors, Inc. and is intended for their exclusive use. This program was developed in conjunction with a grant from U.S. Department of Agriculture and the Food and Drug Administration. It was field tested at the Johns Hopkins Research Centre and was approved for distribution by the Board of Directors, General Motors Corp. at a general meeting on August 15, 1985. General Motors Corp. wholly endorses this program and is making it available to all employees and families. This program will be available at all General Motors Food Service Facilities. It is management's intention to facilitate a wellness and fitness program for everyone.

This program is designed for a target weight loss of 10-17 lbs per week. It will also improve your attitudes and emotions because of its cleansing systematic effects.

The effectiveness of this seven day plan is that the food eaten burn more calories than they give to the body in caloric value.

This plan can be used as often as you like without any fear of complications. It is designed to flush your system of impurities and give you a feeling of well being. After seven days you will begin to feel lighter because you will be lighter by at least 10 lbs. You will have an abundance of energy and an improved disposition.

During the first seven days you must abstain from all alcohol
You must drink 10 glasses of water each day Day One All fruits except bananas.


Your first day will consist of all the fruits you want. It is strongly suggested that you consume lots of melons the first day. Especially watermelon and a loupe. If you limit your fruit consumption to melons, your chances of losing three lbs. on first day are very good.

Day Two: All vegetables. You are encouraged to eat until you are stuffed with all the raw or cooked vegetables of your choice. There is no limit on the amount or type. For your complex carbohydrate, you will start day two with a large baked potato for breakfast. You may top the potato with one pat of butter.

Day Three: A mixture of fruits and vegetables of your choice. Any amount, any quantity. No bananas yet. No potatoes today.

Day Four: Bananas and milk. Today you will eat as many as eight bananas and drink three glasses of milk. This will be combined with the special soup which may be eaten in limited quantities.

Day Five :Today is feast day. You will eat beef and tomatoes. Eat two 10 oz. portions of lean beef. Hamburger is OK. Combine this with six whole tomatoes. On day five you must increase your water intake by one quart. This is to cleanse your system of the uric acid you will be producing.

Day Six: Beef and vegetables. Today you may eat an unlimited amount of beef and vegetables. Eat to your hearts content.

Day Seven :Today your food intake will consist of brown rice, fruit juices and all the vegetables you care to consume.



Tomorrow morning you will be 10-17 lbs. lighter than one week ago. If you desire further weight loss, repeat the program again. You may repeat this program as often as you like, however, it is suggested that you are allowed two glasses of white wine in addition to the instructions on the program. You may substitute champagne for white wine. Under no circumstances are you to drink any other alcoholic beverages with the exception of beer which is allowed. Any liquor (bourbon,vodka, rum) is forbidden. Cream drinks are especially forbidden. You may have an occasional cordial such as creme de menthe or schnapps, but you must always limit yourself to two drinks. If you wine, drink only wine that day. If you have beer, drink only beer that day, etc. Alcohol adds empty calories to your diet. However, after the first week it will help your digestion and settle your stomach.

G.M.'S Wonder Soup:
The following soup is intended as a supplement to your diet. It can be eaten any time of the day in virtually unlimited quantities. You are encouraged to consume large quantities of this soup.

28 oz, Water, 6 Large Onions, 2 Green Peppers, Whole Tomatoes (fresh or canned), 1 Head Cabbage, 1 Bunch Celery, 4 Envelopes Lipton Onion Soup Mix, Herbs and Flavouring as desired.

Additional Comments

Vegetables as may be taken in the form of a salad if desired. No dressing except malt, white or wine vinegar, squeezed lemon, garlic, herbs. No more than one tea spoon of oil.

You have been given a recipe for the WONDER SOUP which can be eaten in unlimited quantities. This soup is a supplement while you are on the program and it should be a pleasure to eat. Not everyone likes cabbage, green peppers, calory etc. This recipe is not inflexible. You may substitute vegetables according to your taste. You may add any vegetables you like: asparagus, peas, corn, turnips, green beans, cauliflower, etc. Try to stay away from beans (lima, pinto, kidney, etc.), however, because they tend to be high in calories even though they are very good for you.

Beverages you may consume while on the program :

Water (flavoured with lemon/lime if desired).
Club Soda is OK.
Black Coffee. No cream or cream substitute. No sugar or sweetness.
Black Tea = Herb or Leaf.
Absolutely nothing else except the fruit juices which are part of day seven. No fruit juices before day seven.
How and Why It Works

Day One you are preparing your system for the upcoming programme. Your only source of nutrition is fresh or canned fruits. Fruits are nature's perfect food. They provide everything you could possibly want to sustain life except total balance and variety.

Day Two starts with a fix of complex carbo-hydrates coupled with an oil dose. This is taken in the morning for energy and balance. The rest of day two consists of vegetables which are virtually calorie free and provide essential nutrients and fibre.

Day Three eliminates the potato because you get your carbohydrates from the fruits. You system is now prepared to start burning excess pounds. You will still have cravings which should start to diminish by day four.

Day Four, bananas, milk and soup sound the strangest and least desirable. You're in for a surprise. You probably will not eat all the bananas allowed. But they are there for the potassium you have lost and the sodium you may have missed the past three days. You will notice a definite loss of desire for sweets. You will be surprised how easy this day will go.

Day Five, Beef and tomatoes. The beef is for iron and proteins, the tomatoes are for digestion and fibre. Lots and lots of water purifies your system. You should notice colourless urine today. Your allowance calls for the equivalent of five "quarter ponders". Do not feel you have to eat all this beef. You must eat the six tomatoes.

Day Six is similar to day five, Iron and proteins from beef, Vitamins and fibre from vegetables. By now your system is in a total weight loss inclination. There should be a noticeable difference in the way you look today, compared to day one.

Day Seven finished off the program like a good cigar used to finish off Victorian meals, except much healthier. You have your system under control and it should thank you for the flushing and cleaning you just gave it.



Sunday, May 23, 2010

Maoist Threat In India






The Communist Party of India (Maoist) is a Maoist political party in India which aims to overthrow the government of India. It was founded on September 21, 2004, through the merger of the Communist Party of India (Marxist–Leninist) People's War and the Maoist Communist Centre of India (MCC). The merger was announced to the public on October 14 the same year. In the merger a provisional central committee was constituted, with the erstwhile People's War Group leader Muppala Lakshmana Rao alias Ganapathi as General Secretary.

The Naxalites, Naxals or Naksalvadis are a Maoist communist group in India, leaders of the Naxalite-Maoist insurgency.

Their name comes from the village of Naxalbari in the Indian state of West Bengal where the movement originated, and the group are far-left radical communists, supportive of Maoist political sentiment and ideology. Their origin can be traced to the split in 1967 of the Communist Party of India (Marxist), leading to formation of Communist Party of India (Marxist–Leninist). Initially the movement had its centre in West Bengal. In recent years, it has spread into less developed areas of rural central and eastern India, such as Chhattisgarh, Orissa and Andhra Pradesh through the activities of underground groups like the Communist Party of India (Maoist).

As of 2009, Naxalites are active across approximately 220 districts in twenty states of India accounting for about 40 percent of India's geographical area, They are especially concentrated in an area known as the "Red corridor", where they control 92,000 square kilometers. According to India's intelligence agency, the Research and Analysis Wing, 20,000 armed cadre Naxalites were operating apart from 50,000 regular cadres working in their various mass organizations and millions of sympathisers, and their growing influence prompted Indian Prime Minister Manmohan Singh to declare them as the most serious internal threat to India's national security.

The Naxalites are opposed by virtually all mainstream Indian political groups. In February 2009, Central government announced its plans for broad, co-ordinated operations in all affected states (Chhattisgarh, Orissa, Andhra Pradesh, Maharashtra, Jharkhand, Bihar, Uttar Pradesh, and West Bengal), to plug all possible escape routes of Naxalites.

India has no one to blame but itself for the rise and growth of the Maoists. Unlike violence by groups like the Lashkar-e-Toiba and the Jaish-e-Mohammed, both tagged with the terrorist label and whose attacks the government can attribute to Pakistan's support, the roots of the Maoists lie squarely in India, in the failure of the Indian state to address extreme poverty in vast stretches of rural India.

Maoist violence is no doubt brutal. It has laid bare the callousness of the Indian state, its failure to deliver good governance and to respond to the plight of the poorest and most marginalized sections of its population.

Analysts are cautioning the government against excessive focus on military methods to deal with a problem that is primarily political.

Recently, Chidambaram said he wanted Maoist-controlled areas to be liberated before any development programs could be launched there. There is concern that this "crackdown first, development later" is wrongly sequenced given the fact that it is the absence of development that has resulted in the emergence and growth of Maoism in the first place. "Development efforts should be an important part of the strategy to defeat them [Maoists]," points out an editorial in Deccan Herald. "To think that they can follow the campaign is to put the cart before the horse."

Mahendra Kumavat, a retired director-general of the Border Security Force who had over a decade's experience in fighting Maoists in the Andhra-Orissa-Chhattisgarh, area says that "the government is going to lose more hearts and minds to the Maoists if it forges ahead with a strike policy that brings nothing but bloodshed and disruption to people in the affected zones". It is "going to multiply our problems, not solve them", he warned.

As India prepares to unleash a war against its own citizens, a campaign is underway to discredit the Maoists. And what better way than to draw parallels with the Taliban? Media reports have described the beheading of the Jharkhand cop as a "Taliban-style killing", while the Maoists were referred to as the "Red Taliban".

Interestingly, this is not the first time that Maoists have decapitated their victims. Ajay Sahni, executive director of the New Delhi-based Institute for Conflict Management argues "it was common for Naxalites [as Maoists are often called in India] of various hues to 'shorten' a man by a foot, 'from the top'. Over the past years, after the formation of the CPI (Maoist), there have been several such incidents [of beheading]."

None of these beheadings were described as "Taliban-style beheadings". It is only after the government decided to take on the Maoists head-on that such analogies have emerged in the media.

Home Ministry officials seem excessively optimistic about the new offensive. "We hope that within 30 days of security forces moving in and dominating the area, we should be able to restore civil administration there," Home Secretary G K Pillai said last week.

Many in India do not think so.

The Maoists might melt away when confronted by the might of the Indian state but they will return to strike back. The Maoists in an earlier avatar were brutally crushed by the Indian state in the early 1960s. They regrouped in subsequent years.

They have indicated that they intend to inflict heavy losses. Describing themselves as "respectable citizens and patriots", they have appealed to the IAF to "not strike at sons and daughters of the soil".

Should the IAF do so, they would "teach the center [the federal government] a lesson that no other revolutionary force has taught them".

"Be prepared for a befitting retribution," the Maoists have warned.

Friday, May 21, 2010

THE BEST ASSUALT RIFLES IN THE WORLD


1


Tavor T.A.R. 21 Standard Version

Tavor, the new Israeli assault rifle is lightweight, compact and ergonomically designed to become an “organic” part of the warfighter. It has already been chosen to arm the Israeli (IDF) and Indian elite troops, and is aggressively marketed worldwide, to become a weapon of choice for future infantry combat suits.

The name “T.A.R. 21” stands for “Tavor Assault Rifle 21st Century”.


•Caliber: 5.56 mm
•Cartridge: 5.56 mm NATO M193/M855 (SS109)
•NET Weight: 3.27 kg (T.A.R.) / 3.18 kg (C.T.A.R.) / 3.67 kg (S.T.A.R.)
•Effective range: 600 m
•In service: 2001 – present


2



SA 80
SA80 (Small Arms for 1980s) is the designation for a revolutionary family of assault weapons. On its introduction, the L85 Individual Weapon (IW) proved so accurate that the Army marksmanship tests had to be redesigned. The British Army uses the L85 Individual Weapon that replaced the rifle and sub-machine gun, and the L86 Light Support Weapon (LSW) that produces higher volumes of fire and is effective at longer ranges. An infantry section consists of two four-man fire teams armed with SA80s: three IWs and one LSW.
The L85 (SA80) is a gas operated, magazine fed, selective fire rifle of bullpup layout. The receiver of the L85 is made from stamped sheet steel, reinforced with welded and riveted machined steel inserts. The gas operated action has a short stroke gas piston, located above the barrel. The gas piston has its own return spring. Gas system has a three-positions gas regulator, one position for a normal firing, second for a firing in adverse conditions and the third for launching the rifle grenades (gas port is shut off). The machined bolt carrier rides inside the receiver on the two parallel steel guide rods, with the single return spring placed above and between the guide rods. The typical rotating bolt has 7 lugs that locks into the steel insert in the receiver, just behind the barrel breech. The charging handle is attached to the right side of the bolt carrier, and prior to A2 upgrade caused some problems by reflecting the ejected cases back into the action, thus causing stoppages. In the L85A2 configuration the charging handle was redesigned to avoid such problems. The charging handle slot is covered by the spring-loaded dust cover. The bolt and its extractor claw also were upgraded in the L85A2, to achieve more reliable extraction of the spent cases.

•Caliber: .223 Rem / 5.56 mm
•Cartridge: 5.56×45 mm NATO
•Weight: 4.7 kg empty / 4.98 kg (with loaded magazine and optical sight)
•Effective range: 400 m
•In service: 1985 – present





3





M16A1 M16A2
Caliber 5.56x45mm (.223 Remington), M193 5.56x45mm NATO / M855
Action gas operated, rotating bolt
Overall length 986 mm 1006 mm
Barrel length 508 mm 508 mm
Weight, empty / loaded w. 30 rounds 2.89 kg / 3.6 kg 3.77 kg / 4.47 kg
Magazine capacity 20 or 30 rounds standard
Rate of fire, cyclic 650 - 750 rounds per minute 800 rounds per minute
Muzzle velocity 945 m/s 975 m/s
Maximum effective range 460 meters 550 meters

The M16 is still a general-issue rifle with the US Armed forces. It is also widely used by the US Law Enforcement agencies, either in military form (for example, the LAPD had some M16s, retired from Army), or in "civilian" semi-automatic only form. The AR-15 style rifles are made in the USA by at least dozen large companies, such as Armalite, Bushmaster, Colt, FN Manufacturing, Hesse, Les Baer, Olympic, Wilson Combat, and by number of smaller companies, many of which do assembly their rifles from components made by some other major manufacturers. M16-type rifles also manufactured outside of the USA, most notably in the Canada, by Diemaco Co. China also makes some AR-15 type rifles at NORINCO state factories. M16 rifles are used by many foreign military groups, most notably the British SAS, who preferred the M16 over the infamous L85A1 rifle, and by many others.

At the present time almost all initial flaws of the M16 are bugged out, and it is considered among the best assault rifles in the world. While its reliability in the harsh conditions cannot match reliability of its main rival, the Kalashnikov AK-47 and AK-74, it is still a quite reliable rifle, especially when well maintained. It is also comfortable to fire and quite accurate.







4



AK-47

Caliber 7.62x39 mm
Action: Gas operated, rotating bolt with 2 lugs
Overall length: 870 mm
Barrel length: 415 mm
Weight, with empty magazine: AK 4,3 kg; AKM 3,14 kg
Magazine capacity 30 rounds (40 rounds box magazines and 75 rounds drums from RPK also may be used)
Cyclic rate of fire 600 rounds per minute

The Kalashnikov assault rifle, also known to the West as the AK-47 (Avtomat Kalashnikova - 47, Kalashnikov automatic rifle, model of 1947), and its derivatives, also known under the common name of AK, is the most prolific small arm of the 2nd half of the XX century. It had been and still is (in more or less modified form) manufactured in dozens of countries, and used in hundreds of countries and conflicts since its introduction. The total number of the AK-type rifles made worldwide during the last 60 years is estimated at 90+ millions. This is a true legendary weapon, known for its extreme ruggedness, simplicity of operation and maintenance, and unsurpassed reliability even in worst conditions possible. It is used not only as a military weapon, but also as a platform for numerous sporting civilian rifles and shotguns (see Saiga semiautomatic shotguns, for example). The AK is an amalgam of previously known features and solutions, combined in the most effective way. The effectiveness, however, depends on the criteria used to measure it, and the key criteria for any and every Soviet and Russian military arm are: Reliability, Simplicity of operation and maintenance, Suitability for mass production. There never was any significant demand for good ergonomics or superb accuracy, though.



5





AK-74 AKS-74 AK-74M
Caliber: 5.45x39 mm
Action Gas operated, rotating bolt with 2 lugs
Weight, empty 3.07 kg 2.97 kg 3.4 kg
Length: 940 mm 940 / 700 mm 942 / 704 mm
Barrel length 415 mm
Rate of fire 600 - 650 rounds per minute
Magazine capacity 30 rounds standard

idea of the reduced caliber ammunition for military shoulder arms was played with for a very long time. Each time the technology leaped forward, the standard calibers were reduced - from the 0.45 - 0.50 inch (11.4 - 12.7mm) of the mid-1800 to the .30 of the mid-1900s. The idea of further reduction of the caliber down to 6.5 - 5.6 mm (.240 - .220 inch) was also considered in many countries since the beginning of the XX century, but it was not until the 1960s when the idea of the low impulse, small-caliber, high velocity round came up to something real. When US Army adopted the M16 rifle in the mid-1960s, everybody else eyed Americans with interest. And as soon as the idea of small caliber rifle was found worthwhile, the total rearming began.

Soviet army started the development of its own small-caliber ammunition in the early 1960s. After some years of development, a new round was created. This round featured a bottlenecked, tapered case 39mm long made of steel, loaded with slim, relatively long bullet with nominal caliber of 5.45mm (actual bullet diameter is 5.62 mm). The bullet featured a combined steel and lead core with the hollow nose, muzzle velocity from the 415mm barrel was about 900 m/s. It must be noted that the new 5.45mm ammunition featured a new case of smaller diameter (compared to 7.62x39 M43 cartridges); this allowed for lighter round and also solved the problem of loading of the 7.62mm ammunition into the 5.45mm weapon by mistake (which otherwwise might result in a catastrophical failure of the weapon).
As soon as the new ammunition was available and accepted by the Soviet Military, it was decided to develop a new family of small arms around this cartridge, and an official requirements for new family of small arms were issued to all development organizations in 1966. Trials of new weapons commenced in 1968, and it must be note that most rifles, submitted for trials, were of highly advanced designs, as the main goal of the new weapon was to significantly improve hits probability (compared to 7.62mm AKM rifles). Most weapons were build using so called "balanced action", in which additional mass is added to the action to counter-recoil synchronously with the bolt group, to minimize its effect on the gun stability. About the only weapon of the more or less conventional design was the entry by Kalashnikov team - this was more or less the old AKM rifle, adapted for new 5.45mm ammunition.



6




INSAS

Caliber: 5.56x45 mm NATO
Action: Gas operated, rotating bolt
Overall length: 945 mm with fixed butt; 960 / 750 mm with folding butt
Barrel length: 464 mm
Weight: 3.2 kg empty
Rate of fire: 650 rounds per minute
Magazine capacity: 20 or 30 rounds

Since late 1950s, Indian armed forces were equipped with 7.62mm NATO L1A1 slef-loading rifles, which were licensed copies of the famous Belgian FN FAL rifle. As the 7.62mm self-loading rifles started to become obsolete by the 1980s, India began to develop the INSAS (Indian National Small Arms System), which incorporated features from several popular foreign designs. The INSAS system was originally planned to have three components - a standard rifle, a carbine, and a squad automatic rifle (LMG), all chambered for 5.56 x 45 NATO ammunition. In 1997 the rifle and LMG were ready for mass production, and in 1998 the first units were observed on an Independence Day parade armed with INSAS rifles. The mass introduction of the INSAS rifle was initially delayed by the lack of the domestically made 5.56 mm ammunition and India accordingly bought significant stocks of ammunition from the Israeli IMI company. At the present time at least 300,000 INSAS rifles are in service with the Indian army; some of these have seen action in Indo-Pakistani conflict. The INSAS rifles are made by the Ishapore Rifle Factory.

The INSAS rifle is broadly based on the famous Kalashnikov AK-47 action, but with many modifications. The basic gas-operated action with long stroke gas piston and a rotating bolt, as well as the stamped steel receiver, are generally the same as in modern Kalashnikov rifles. However, the gas system is fitted with a manual gas regulator, similar in design to that found on FN FAL rifles, as well as a gas cutoff. The charging handle has been moved from the bolt carrier to the left side of the forearm; it is similar in position and design to German HK G3 rifle. The selector / safety switch is located at the left side of the receiver, above the pistol grip, and allows for single shots and three round bursts. The rifle is fitted with a side-folding carrying handle, and either a solid or side-folding metal buttstock. Furniture can be made from wood or polymer. Standard magazines are made from semi-translucent polymer and contain 20 rounds. Longer 30-round magazines of similar design are available for the INSAS LMG but can also be used in the rifle. The sights consist of a hooded front, mounted on top of the gas block, and a diopter rear, mounted on the receiver cover. The flash hider is shaped to accept NATO-standard rifle grenades. INSAS rifles can be fitted with AKM-style multipurpose knife-bayonets.


7



QBZ-97 / Type 97
5.56x45mm QBZ-97 / Type 97 assault rifle; note different magazine port, designed to accept STANAG / M16-type magazines
Data for QBZ-95 (QBZ-97 in parenthesizes, where differs from QBZ-95)
Caliber: 5.8x42 mm (5.56x45 mm NATO)
Action: Gas operated, rotating bolt
Overall length: 760 mm
Barrel length: 520 mm
Weight: 3.4 kg unloaded
Rate of fire: ~ 650 rounds per minute
Magazine capacity: 30 rounds
In the late 1980s Chinese designers developed a 5.8 x 42 cartridge, apparently designated DBP87, which is claimed to be superior to both the 5.56 mm NATO and the 5.54 mm Soviet. This cartridge develops a muzzle velocity of 930 metres per second from a standard barrel, with a bullet weighing 4.26 gram.

As soon as the ammunition was ready, the PLA began to develop an entirely new and much more modern family of small arms based on the same action. This family, known as QBZ-95 ('Qing Buqiang Zu' = Light Rifles family, 1995), was first displayed outside the PLA in 1997, when China took over Hong Kong; it was observed that the Chinese guards were armed with a new, modern looking bullpup rifle. In fact it is one of an entirely new family of weapons, all designed around the same action and bullpup layout, which include the assault rifle, a shorter carbine, a light support weapon (with a bipod, a heavier barrel and large capacity magazine), and a sniper rifle. While being quite similar inside, these guns have different body shapes and cannot be converted from one configuration to another. The QBZ-95 line of weapons is now spreading throughout the PLA, commencing with elite units.

The QBZ-95 is a gas operated, magazine fed, automatic weapon with a bullpup layout. It has a short stroke gas piston and a rotating bolt. The charging handle is located at the top of the receiver, under the carrying handle. The housing is made from polymer, with an integral carrying handle, which holds the rear sight base, and has mounting points for optical or night vision scopes. The ejection port is made only at the right side of the weapon, so it cannot be fired from the left shoulder. Standard sights are of the open type, graduated from 100 to 500 metres. The front part of the barrel in the standard version is left unobstructed, so the QBZ-95 rifle can be used to launch rifle grenades. It also can be fitted with an underbarrel grenade launcher or with a knife bayonet. A compact carbine version, sometimes referred to as the CAR-95, cannot use either a grenade launcher or a bayonet, because of the much shortened barrel. Fire controls of QBZ-95 rifle consist of a trigger and a safety/selector switch, located (quite inconveniently) at the rear left of the receiver, behind the magazine housing. QBZ-95 can fire single shots or bursts.

The export version, QBZ-97, which is chambered for popular 5.56 x 45 NATO ammunition, is internally similar to QBZ-95, but has a different, much deeper magazine housing, which accepts a NATO-standard (M16-type) magazines.




8




FN2000
Caliber: 5.56x45 mm NATO
Action: Gas operated, rotating bolt
Overall length: 694 mm
Barrel length: 400 mm
Weight: 3.6 kg empty, in standart configuration; 4.6 kg with 40mm grenade launcher
Magazine capacity: 30 rounds (any NATO / STANAG type magazines)

During the late 1980s and early 1990s famous Belgian company FN Herstal began the search for its next entry into the assault rifle world. The aim this time was to produce a modern, modular weapon, and this ultimately resulted in the FN F2000 rifle, which was first displayed in public in 2001. The F2000 offers all of the most popular features of the modern assault rifle, such as a compact bullpup layout, completely ambidextrous handling, and a modular design with plenty of options and add-ons already available, which allow the rifle to be “tailored” for any particular mission or tactical situation. For example, for peacekeeping operations F2000 could be fitted with less-lethal M303 underbarrel module, which fires tear gas or marker projectiles using pre-compressed air. On the other hand, the F2000 could be fitted with various 40 mm FN EGLM grenade launchers and a proprietary computerized fire control system, instead of the standard low-magnification optical sights. So far FN F2000 rifle found only few buyers, including Armed forces of Slovenia and Belgian Special operations forces. Nevertheless, it is one of most promising assault rifles on the market.
Quite recently FN also introduced a civilian version of F2000, known as FS2000. It has a somewhat longer barrel and is limited to semi-automatic fire. Otherwise it is the same excellent weapon, with great ergonomics and 100% ambidexterity.

The F2000 rifle is a gas operated, rotating bolt, selective-fire weapon, featuring a polymer stock with a bull-pup layout. It utilizes a short-stroke gas piston and a 7-lug rotating bolt which locks into the barrel extension. The unique feature of the F2000 rifle is its patented front ejection system: the spent cases, extracted from the chamber, travel from the rear part of the gun to the ejection port near the muzzle via a special ejection tube and fall out of the gun at the safe distance from the shooters' face. This is achieved using a special swinging guide, which enters the way of the closing bolt, and directs the spent case, which is held on the bolt face, to the ejection tube, while, at the same time, lower lugs of the bolt are stripping a fresh cartridge from the magazine. The cocking handle is mounted well forward on the left hand side, just above the fore grip, and it can easily be operated with the right hand when the gun is held left-handed. The selector switch is mounted at the bottom of the trigger guard. All of these features combine to make the F2000 the first genuinely ambidextrous bullpup, able to be used with equal ease by right and left handed shooters without requiring any adjustments. In its standard configuration, the F2000 is perfectly balanced around the pistol grip.
The stock has built-in standard rails on the top of the weapon (for different sights and scopes etc) and a mounting point ahead of trigger guard, where additional modules may be installed (such as grenade launchers, non-lethal modules etc). In the basic configuration, the upper rail mount is fitted with a 1.6X magnification optical sight, and the lower mounting point is covered by a removable handguard. At the current time, the F2000 rifle may be upgraded, depending on the mission, with FN's 40 mm low-velocity grenade launcher (on the lower mount, instead of the handguard), or with M303 non-lethal module; other options are handguards with built-in laser pointers or flashlights. The standard low-magnification combat scope, which has a back-up open sights on its top cover, may be replaced by any other scope on Piatiny-style mount, or with FN's proprietary computerized fire control module with laser rangefinder, for both the rifle and 40 mm grenade launcher.



9



FN SCAR-H / Mk.17
7.62mm NATO FN SCAR-H / Mk.17 rifles of current (2007/2008) production, top to bottom in Long Barrel (LB), bstandard (Std) and Close Quarter Combat (CQC) configurations
Image: FNH USA

Mk.16 SCAR-L (Light) Mk.17 SCAR-H (Heavy)
Caliber 5.56x45 NATO 7.62x51 NATO basic
7.62x39 M43 and others additionally
Overall length, standard configuration 850 mm (max) / 620 mm (min) 997 mm (max) / 770 mm (min)
Barrel length 254mm/10" (CQC), 355mm/14" (Std), 457mm/18" (LB) 330mm/13" (CQC), 406mm/16" (Std), 508mm/20" (LB)
Weight 3.5 kg empty 3.86 kg empty
Rate of fire 600 rounds per minute 600 rounds per minute
Magazine capacity 30 rounds standard 20 rounds (7.62x51 NATO)
30 rounds (7.62x39 M43)


The US Special Operations Command (US SOCOM) issued a solicitation for the procurement of SOF Combat Assault Rifles (SCAR) on October 15th, 2003. This solicitation requested a new combat rifle, specially tailored for the current and proposed future needs of the US Special Forces, which are somewhat different from latest generic US Army requirements, which are being fulfilled by the newest Heckler-Koch XM8 assault rifle. The key difference in basic requirements between XM8 and SCAR is that, while XM8 is a single-caliber weapon system, tailored for 5.56x45mm NATO ammunition, the SCAR should be available in various different calibers. Initial SOF requirements included two basic versions of SCAR system - the SCAR Light (SCAR-L), available in 5.56mm NATO, and the SCAR heavy (SCAR-H), which should be initially available in significantly more powerful 7.62x51 NATO chambering, and should be easily adaptable in the field to other chamberings. These other chamberings initially include the well-spread 7.62x39 M43 ammunition of the Soviet / Russian origins, and probably some others (like the proposed 6.8x43 Remington SPC cartridge, especially developed for US Special Forces). The key idea of SCAR rifle system is that it will provide the Special Forces operators with wide variety of options, from short-barreled 5.56mm SCAR-L CQC variation, tailored for urban close combat, and up to long range 7.62x51 SCAR-H Sniper variant, as well as 7.62x39 SCAR-H, which will accept "battlefield pickup" AK-47/AKM magazines with 7.62 M43 ammunition, available during the operations behind the enemy lines. Both SCAR-L and SCAR-H shall be initially available in three versions, Standard (S), Close Quarters Combat (CQC) and Sniper Variant (SV; now it is dubbed Long Barrel - LB). All these variants, regardless the caliber and exact configuration, will provide the operator with the same controls layout, same handling and maintenance procedures, and same optional equipment, such as sights, scopes, and other current and future attachments.


As it turned out, FN SCAR rifles are not based on any previous weapons but designed from the scratch. In all variants FN SCAR rifles feature gas operated, short stroke piston action with rotating bolt locking. Bolt system appears to be somewhat similar to that of FN Minimi / M249 SAW machine gun. This system apparently is less sensitive to fine sand, dust and any other fouling inside the receiver, than any system with M16-type multi-lug bolt and plunger-type ejector.

Mk.16 SCAR-L rifle will use improved M16-type magazines, made of steel; Mk.17 SCAR-H will use proprietary 20-round magazines in 7.62x51 NATO chambering, or standard AK-type magazines in proposed 7.62x39 M43 chambering. Current prototypes of SCAR rifles do not have bayonet mounts, and, probably, will never have one.



10





FAMAS F1 FAMAS G2
Caliber 5.56mm NATO (.223rem)
Action Delayed blowback
Overall length 757 mm
Barrel length 488 mm
Weight 3.61 kg with empty magazine 3.8 kg with empty magazine
Magazine capacity 25 rounds (proprietary) 30 rounds (STANAG)
Muzzle velocity 960 m/s 925 m/s
Rate of fire 900-1000 rounds per minute 1000-1100 rounds per minute
Effective range 300 meters 450 meters

FAMAS stands for Fusil d'Assaut de la Manufacture d'Armes de St-Etienne (Assault Rifle by St-Etienne Arms Factory - a member of the French govt. owned GIAT Industries concern). Development of this rifle began in 1967, under the leadership of the Paul Tellie, a French arms designer. This new rifle was intended to replace in service the MAS Mle.49/56 semi-automatic rifles, MAT-49 submachine guns and some MAC Mle.1929 light machine guns. First FAMAS prototype had been built in 1971. French military began to test this rifle in 1972-73, but, in the meantime, France adopted a Swiss-designed SIG SG-540 5.56mm assault rifle as an intermediate solution. FAMAS rifle was adopted by the French in 1978 and since then became a standard French Army shoulder fired small arm, known among the French soldiers as "Le Clairon" (the bulge). According to the Janes Infantry Weapons 2000, the total number of FAMAS F1 rifles built is estimated at 400 000, and the production of the F1 variant is now completed. It is still used by the French army, and was exported in small numbers to some countries like the Senegal or United Arab Emirates. Since then, the GIAT Industries developed an improved version of the F1, known as the G1. This rifle featured an enlarged trigger guard, that covered a whole hand, and a slightly improved plastic handguards. G1 was an intermediate design, and was consequently replaced by the latest production model, the FAMAS G2, which appeared circa 1994. This rifle has the G1-style enlarged trigger guard but can accept only STANAG type (M16-compatible) magazines. It was adopted and purchased by the French Navy in the 1995, with the French Army soon following the suit, and also offered for export. At the present time the slightly upgraded FAMAS G2 rifle is used as a platform for the future FELIN system (a French counterpart to the US "Land Warrior" programme), which incorporates a various electronic sights and sensors, connected to the soldier carried equipment, like the helmet mounted displays, ballistic and tactical computers etc. GIAT also now offers some variations of the basic FAMAS G2 rifle, such as "Submachine gun" with shortened receiver and barrel of 320 mm long, "Commando" with the standard receiver and the 405 mm barrel, and the "Sniper", with longer and heavier 620 mm barrel and an integral scope mount instead of the carrying handle.

The FAMAS rifles seen some action during the operation "Desert Storm" in Kuwait in 1991, as well as in some peace-keeping operations in the mid and late 1990s, and proved itself as a reliable and trustworthy weapons.




11




G36 G36K G36C
Caliber 5.56x45mm (.223 Rem)
Length (buttstock open / folded) 998 / 758 mm 860 / 615 mm 720 / 500 mm
Barrel length 480 mm 320 mm 228 mm
Weight empty 3.6 kg (3.3 kg G36E) 3.3 kg (3.0 kg G36KE) 2.8 kg
Magazine capacity 30 rounds standard
Rate of fire 750 rounds per minute


The Heckler und Koch G-36 assault rifle had been born as HK-50 project in early 1990s. The reason behind that project was that the Bundeswehr (the German army), after the cancellation of the G11 and G41 projects, was left with outdated G3 rifle and no modern rifle, compatible with the current NATO standards at hands. Therefore the famous company Heckler & Koch was set to develop a new assault rifle for both German army and the export. The new 5.56mm assault rifle has been adopted by the Bundeswehr in the 1995, and in the 1999 the Spain adopted its slightly different, export version, G36E as its standard infantry rifle. The G36 also found its way into the hands of various law enforcement agencies worldwide, including British police and some US police departments. So far I've heard very few complaints about this rifle, and a lot of good revives and opinions. In fact, the only complaints about G36 that I know are the overheating of the handguards during the sustained fire, and the loose of zero of built in scope on some G36KE rifles, used by US police. Some German soldiers also complained about position of dual optical sights and those sights being easily fogged in bad weather (rain or snow). Otherwise it is a good rifle, accurate, reliable, simple in operations and maintenance, and available in a wide variety of versions - from the short-barreled Commando (some even said that it's a submachine gun) G36C and up to a standard G36 rifle. The MG36 squad automatic weapon (light machine gun), which was initially designed as a heavy-barreled version of the G36, was in fact a short-lived proposition that never went into mass production.

The G36, in severely modified form, was used as a "kinetic energy" part of the now-cancelled US XM-29 OICW weapon and it also served as a base for XM8 assault rifle (also cancelled).

Mountaineering :The best way to adapt with land

1.NEHRU INSTITUTE OF MOUNTAINEERING,INDIA

Category:Sports & Recreation - Outdoor Sports
Description:NIM has completed 40 years of existence. Training Mountaineers has always been raisen d'etre of this Institute. Over the years, thousands of Indians and hundreds of Foreigners have passed through the portals of this great Institution.
Although one of the youngest Institute of India, it has today striven forth to become India's 'sheet anchor ' in the field of mountaineering. The demanding and stringent training standards, excellent administration, unflinching loyalty, dedication and competency of the staff, has put NIM not only as the foremost Institution of India, but also one of the finest in the world.
The aim of the Institute is to introduce and initiate young men, women and school children to the mountains and nature through its various Mountaineering and Adventure training courses. Special emphasis is laid on instilling the concept of Adventure sports, without causing environmental degradation.
The legendary Polish climber (late) Wanda Rutkiewicz during her visit to the Institute remarked. "The Mecca of Indian Mountaineering and un-questionably India's pride in the mountaineering world".
Although one of the youngest Institute of India, it has today striven forth to become India's 'sheet anchor ' in the field of mountaineering. The demanding and stringent training standards, excellent administration, unflinching loyalty, dedication and... (read more)

Contact Info
Email:nimutk2004@sancharnet.in.
Website:http://www.nimindia.org/
Location:Uttarkashi, India.

1. ELIGIBILITY
a) ADVANCE MOUNTAINEERING COURSE is for trainees Graded 'A' only in Basic Mountaineering course from NIM Uttarkashi, HMI Darjeeling, JIM Pahalgam, (J&K), ITBP Training Centre Auli, MAS Manali and SGMI Gangtok.
b) SEARCH & RESCUE and METHOD OF INSTRUCTION COURSES are for trainees Graded 'A' only in Advance Course.
2. ADMISSION TO FOREIGNERS
To report to the Principal one day in advance along with the Passport and valid Visa for direct admission into a course, 250 US dollars for adventure course and 650 US dollars each for remaining courses is to be paid as course fee.
3. PHYSICAL FITNESS LEVEL
a) Trainees should be in good physical condition prior to undertaking any course. Taking long walk on uneven tracks with load is preferable. Long distance running and regular fingers and arms exercise will prove to be helpful.
b) Search & Rescue course requires a high level of fitness.
c) A test to qualify 15 kms trek with 15-17 kg load, may be taken before a trainee is accepted in the Basic Mountaineering Course.
4. SUBSIDISED FEE FOR INDIAN TRAINEES
a) Training fee should be remitted through a Bank Draft payable at State Bank of India/Punjab National Bank, Uttarkashi in favor of NIM, Uttarkashi. PART PAYMENT, CHEQUES, MONEY ORDERS WILL NOT BE ACCEPTED.
b) Fee includes expenses on food, accommodation, equipment, transportation, medicines and other training expenses during the course.
5. REFUND OF FEE
Cancellation of seat 2 MONTHS earlier entitles refund of fee with 25% deduction.
6. ARMED FORCES & PARA MILITARY PERSONNEL
Serving Armed forces, Para Military and NCC Personnel, should apply through their respective Service Headquarters and Departmental Channels. They can however apply as private trainees.
7. TRANSFER OF SEAT
Request of transfer of seat on compassionate ground may be considered only once. No Refund of fee is permitted thereafter.
8. ARRIVAL
Trainees must arrive an evening before commencement of the course. LATE ARRIVALS EVEN BY ONE DAY WILL NOT BE PERMITTED TO JOIN THE COURSE.
9. RAILWAY CONCESSION FORM
Return railway concession form may be given to a trainee on request from Rishikesh railway station to nearest station of his/her home place after reporting to this institute.
10. NIM PROSPECTUS
a) NIM Prospectus which has the Application Form is available on payment of Rs. 100/- through a Bank Draft, payable at SBI/PNB, Uttarkashi in favor of NIM Uttarkashi. Prospectus is normally forwarded though ordinary post i.e. Book Post For Registered Post, a self addressed.
b) Application Forms are to be sent in original along with a photograph, XEROX COPIES OF FORMS ARE NOT ACCEPTED.
COLONEL M.M.MASUR
PRINCIPAL, NIM


11.Jawahar Institute of Mountaineering and Winter Sports

The Jawahar Institute of Mountaineering and Winter Sports (JIM or JIMWS) was established near Pahalgam (at Aru) in J&K in October 1983. However after 1989, due to disturbances in the valley, students were reluctant to come to Aru for training. Accordingly, it was decided to shift the Institute temporarily to Batote on the Jammu side of Banihal in August 1990. However, in view of certain adverse reports regarding law & order, regular training courses conducted by the Institute were temporarily suspended from April 1996. The Institute is now (2006) based out of Nunwan (famous for where the Pahalgam Amarnath Yatra camp is organized at - a couple of kms short of Pahalgam), in Pahalgam and is back to conducting regular courses.

contactinfo:Principal Jawahar Institute of Mountaineering & Winter Sports, P O Tringla, Batote 182 143 Tel (O) (01998) 4120 Fax (O) (01998) 4334

111.Himalayan mountaineering institute

Col Neeraj Rana
Principal
HIMALAYAN MOUNTAINEERING INSTITUTE
Darjeeling-734101(WB), INDIA
Tel: +91 354 2254083 / 2254087 / 2270158
Fax: +91 354 53760 / 54330
Email: hmi_slg@sancharnet.in
hmi_darj@rediffmail.com
ranamikey1@gmail.com

Thursday, May 20, 2010

BEST FIGHTER HAWKS IN THE WORLD



1





Rafale
Dassault Rafale Specifications
Primary Function: Multi-role fighter / reconn.
Contractor: Dassault
Crew: Single or twin seater
Unit Cost: N/A
Powerplant
Two SNECMA M88-3 turbofans each rated at 19,555 lb (86.98 kN) with afterburning - Rafale C
Dimensions
Length: 50 ft 3 in (15.3 m)
Wingspan: 35 ft 9 in (10.9 m)
Height: 17 ft 6 in (5.34 m)
Weights
Empty: N/A
Maximum Takeoff: 47,399 lb (21500 kg) -- Rafale C
Performance
Speed: Maximum level speed 'clean' at 36,090 ft (11000 m) 1,321 mph (1,147 kt / 2125 km/h) -- Rafale C
Ceiling: 60,000 ft
Range: 1000 nm
Armament
Cannon: 1 30mm DEFA 554; Mica, R.550 Magic 2, BGL 400

2




F22 Raptor
F-22 Raptor Specifications
Primary Function: Fighter, air dominance
Contractor: Boeing and Lockheed Martin
Crew: Model F-22A will carry one crewperson
Unit Cost: N/A
Powerplant
Two Pratt & Whitney F119-PW-100 engines (155.69 kN / 35,000 lb st with afterburning each)
Dimensions
Length: 62 ft 1 inch
Wingspan: 44 ft 6 inches
Height: 16 ft 5 inches
Weights
Empty: N/A
Maximum Takeoff: 60,000 lb (27216 kg)
Performance
Speed: Mach 2 class
Ceiling: 50,000 ft (15240 m)
Range: N/A
Armament
One internal M61A2 20-mm cannon, three internal weapons bays, underside bay for four AIM-120A AMRAAMs and two lateral intake bays each with two AIM-9M sidewinder AAMs. Revised bays for 1,000 lb JDAMs replacing two AIM-120s and AIM-9X AAMs. Four underwing stores stations with provision for two AGM-137A Tri-Service Standoff Arrack Missiles and / or fuel tanks.



3



X 35 Joint strike

X-35 Joint Strike Fighter Specifications
Primary Function: Strike fighter [Conventional Takeoff and Landing]
Contractor: Lockheed-Martin
Crew: One
Unit Cost (FY94$) $28M
Powerplant
One Pratt & Whitney F119-PW-100 derivative from F-22 Raptor
Dimensions
Length: 45 feet
Wingspan: 36 feet
Height: N/A
Weights
Empty: 22,500 lbs
Maximum Takeoff: 50,000 lbs
Performance
Speed: supersonic
Ceiling: N/A
Combat Radius: over 600 nautical miles
Armament
N/A

X-35 Specifications
Primary Function: Strike fighter [Short Takeoff and Vertical Landing]
Contractor: Lockheed-Martin
Crew: One
Unit Cost (FY94$) $35M
Powerplant
One Pratt & Whitney F119-PW-100 derivative from F-22 Raptor
Dimensions
Length: 45 feet
Wingspan: 36 feet
Height: N/A
Weights
Empty: 22,500 lbs
Maximum Takeoff: 50,000 lbs
Performance
Speed: supersonic
Ceiling: N/A
Combat Radius: over 600 nautical miles
Armament
N/A

4



SU 37 Flanker

Su-37 Flanker Specifications
Primary Function: Air superiority fighter
Contractor: Sukhoi Design Bureau
Crew: One
Unit Cost: N/A
Powerplant
Two Lyulka AL-37FU vectored-thrust afterburning turbofans, 30,855 lb thrust each
Dimensions
Length: 21.94 m (72 ft)
Wingspan: 15.16 m (49 ft 9 in)
Height: 6.84 m (22 ft 5 in)
Weights
Empty: N/A
Maximum Takeoff: 34,000 kg (74,960 lbs)
Performance
Speed: 2,500 km/h (1,553 mph / 1,350 Kts / mach 2.35) -- altitude
1,400 km/h (870 mph / 756 Kts / mach 1.32) -- sea level
Ceiling: 59,055 ft
Range: 1,390 km (863 mi / 750 nm) -- low altitude at 497 mph
3,300 km (2,051 mi / 1,782 nm) -- high altitude at 590 mph
Climb Rate: 230 m/sec (45,300 ft/min)
Armament
One GSh-30-1 30mm cannon, plus up to 18,075 lb including R-73/R-77 AAMs, AGMs, bombs, rockets, drop tanks, and ECM pods carried on fourteen external points
5


Su -30
Dimensions:Height6.355mWingspan 14.70mSpan of Foreplane 6.40mLength Excluding Probes23.335mWeights:Empty Weight 17,700kgFuel5,090kgMaximum Fuel 9,400kgTake-off Weight 26,090kgMaximum Take-off Weight 38,000kgMaximum External Payload8,000kgEngines:Type2 x Saturn AL-37FP thrust vectoring enginesThrust83.4kNThrust With Afterburn142.2kNPerformance:Maximum Level Speed 2.35 Mach, 2,150km/hrMaximum Rate of Climb 13,800m/minMaximum Altitude17,500mCombat Range 3,000kmRange With Single In-flight Refuelling5,200kmTake-off Run550mLanding Run 670m



6



Eurofighter Typhoon
Eurofighter Specifications
Primary Function: Fighter
Contractor: Germany, Italy, Spain, UK
Crew: Pilot
Unit Cost: N/A
Powerplant
Two EJ200 Turbofan Engines rated at 20,000 lbf (90 kN) afterburning each
Dimensions
Length: 49.08 ft
Wingspan: 35.93 ft
Height: 5.28m
Weights
Empty: 21,495 lb (approx.)
Maximum Takeoff: 46,297 lb (approx.)
Performance
Speed: 1,320 mph (2125 km/h)
Ceiling: 60,000 ft
Combat Radius: air defence with 10-min loiter : 1389 km
Armament
Internally mounted 27mm Mauser gun; Mix of Beyond Visual Range Air-to-Air Missiles (BVRAAM) and Short-Range Air-to-Air Missiles (SRAAM) carried externally; Four BVRAAM under fuselage in semi-conformal carriage configuration; Laser guided bombs; Advanced anti-armour weapons; Conventionally armed stand-off missiles
Service Life
First Flight: August 1986 (prototype)
March 27, 1994 (EF-2000)
End of Service: N/A
Number Built: [~698 in production]


7



F-18 super Hornet

Both the single seat E and two-seat F models convert quickly from one mission type to the next with the flip of a switch to provide consistent air dominance:

Day/night strikes with precision-guided weapons
Anti-air warfare
Fighter escort
Close air support
Suppression of enemy air defense
Maritime strike
Reconnaissance
Forward air control
Tanker
Payload FlexibilityThe Super Hornet's versatility applies to its weapon stations and payload types:

11 weapon stations
Supports a full complement of smart weapons, including laser-guided bombs
Carries a full spectrum mix of air-to-air and air-to-ground ordnance
Power and Flight CharacteristicsThe Super Hornet is powered by two General Electric F414-GE-400 engines:

Distinctive caret-shaped inlet to provide increased airflow and reduced radar signature
22,000 pounds (98 Kn) of thrust per engine, 44,000 pounds (196 Kn) per aircraft
Flight qualities:

Highly departure resistant through its operational flight envelope.
Unlimited angle-of-attack and carefree flying qualities for highly effective combat capability and ease of training.
Reconfigurable digital flight-control system detects and corrects for battle damage.
UpgradeabilityLong-term designed in versatility ensures the Super Hornet's investment value. Current upgrades delivered in the Block Two configuration include:

Active electronically scanned array (AESA) radar
Advanced targeting forward-looking infrared (ATFLIR) system
Joint-helmet mounted cueing system (JHMCS)
Multifunctional information distribution system (MIDS)
Advanced aft crew station
Fibre channel switch for increased data processing capability
Fully integrated weapons systems and sensors for reduced crew workload and increased capability.

8




MiG -35
Key Data:Crew1-2ManufacturerMikoyanFirst Flight2007Number Built10 as of 2008Developed FromMiG-29MDimensions:Length19m (62ft 4in)Wingspan15m (49ft 3in) Height6m (19ft 8in)Weights:Empty Weight11,000kgLoaded Weight17,500kgMaximum Take-Off Weight29,700kgEngines:Powerplant2 × Klimov RD-33MK afterburning turbofansDry Thrust5,400kgf, 53.0kN (11,900lbf) eachThrust with Afterburner9,000kgf, 88.3kN (19,800lbf) eachPerformance:Maximum speedMach 2.5 (2,400km/h, 1,491mph) at altitudeRange2,000km Ferry Range3,100kmService Ceiling17,500m Rate of Climb330 m/s (65,000 ft/min)Thrust / Weight1.14





9


MiG -29
Key Data:Crew1 - pilotDimensions:Length17.32mHeight4.73mWingspan11.36mWeights:Normal Take-Off Weight14,750kgMaximum Take-Off Weight17,720kgMaximum Weight Combat Load3,000kgMaximum Fuel4,300kgEngines:Engine2 x turbofan RD-33 enginesThrust8,300kgPerformance:Maximum Speed Near Ground1,500km/hMaximum Speed at Altitude2,400km/hService Ceiling18,000mFlight Range Near Ground700kmFlight Range at Altitude1,500kmTake-Off Thrust-to-Weight Ratio1:12Maximum Operatioal G-Load9gAir Target Detection Range60kmR-73 Air-to-Air Missile:Maximum Launch Weight105kgWarhead7.3kg, rod typeGuidanceCooled infraredLength2.9mDiameter0.17mFin Span0.51mMaximum Launch Range20kmMinimum Range of Aft Hemisphere Launch300mTarget Acceleration g-Load12gKill Probability Against a Fighter Target0.6Maximum Target Speed2,500km/hTarget Altitude0.02km to 20kmR-27 Medium-Range Missile:Guidance System R-27R/TSemi-active radar / infraredMaximum Launch Range R-27R/T41km / 32kmLaunch Weight R-27R/T253kg / 245kgDimensions (Length x Diameter x Fin Span) R-27R/T4.08m x 0.23m x 0.97m / 3.8m x 0.23m x 0.97mWarhead39kg, rod typeTarget g-Load8gFighter Aircraft Target Kill Probability0.7Maximum Target Speed3,500km/hTarget Altitude0.02km to 27kmMaximum Vertical Separation Carrier Aircraft to Target10kmR-60 Short-Range Air-to-Air Missile:ManufacturerVympelMaximum Launch Range10kmGuidance SystemInfrared, with photo detector coolingWarhead3.5kg, rod typeLength2.09mDiameter0.12mFin Span0.39mKill Probability Against a Fighter0.5Target g-Load12gMaximum Target Speed2,500km/hTarget Altitude0.03km to 20km


10



F -16
Dimensions:Wingspan 10m Length 15m Height 5m Weights:Empty Weight 8,500kg Engines:Type1 x P&W F100-PW-200/220/229 or General Electric F110-GE-100/129Thrust29,000lbPerformance:Maximum Speed 1,500mph (Mach 2)Maximum Altitude In excess of 15,000m (50,000ft)RangeMore than 2,000 miles ferry range (1,740nm)g limit In excess of 9g

know the hawks around you



History of Aviation

I. INTRODUCTION

Aviation is defined as the design, manufacture, use, or operation of aircraft - in which the term aircraft refers to any vehicle capable of flight. Aircraft can either be heavier-than-air or lighter-than-air: lighter-than-air craft including balloons and airships, and heavier-than-air craft including airplanes, autogiros, gliders, helicopters, and ornithopters.

For centuries man has dreamed to soar with the birds. Famous inventors such as Leonardo da Vinci, John Stringfellow, and Lawrence Hargrave have conjured up ideas of how to get some of the strangest machines to fly long before the Wright brothers' famous first flight at Kitty Hawk.


II. EARLY AVIATION

The first form of an aircraft was the kite, designed in the 5th century BC. Later on in the 13th century, Roger Bacon, an English monk, performed studies which later gave him the idea that air could support a craft just like water supports boats. In the 16th century, Leonardo da Vinci studied birds' flight, and later produced the airscrew and the parachute. The airscrew, leading to the propeller later on, and the parachute were tremendously important contributions to aviation. He envisioned three different types of heavier-than-air craft: the helicopter, glider, and ornithopter (a machine with mechanical wings which flap to mimic a bird). Although Leonardo's designs were impractical, seeing they required human muscular power which was insufficient to generate flight with the aircraft he envisioned, he was vital to aviation because he was the first to make scientific suggestions.


III. THE 19TH CENTURY

Some of the more credible developments in actual flight and stability occurred in the 19th century. British Sir George Cayley designed a combined helicopter and horizontally propelled aircraft, and British Francis Herbert Wenham used wind tunnels in his studies and predicted the application of multiple wings placed above each other. Another famous inventor was John Stringfellow, who designed a steam-engine powered aircraft which was launched from a wire. This model demonstrated lift but failed to actually climb. Lawrence Hargrave, a British-born Australian inventor, created a rigid-wing aircraft with flapping blades operated by a compressed-air motor; it flew 312 ft (95m) in 1891. A famous glider developer in the 19th century was Jean Marie Le Bris, a Frenchman who tested a glider with movable wings.

Kites also played an important role in the development of aviation: they could be used to test aerodynamics and flight stability. Lawrence Hargrave first created the box kite in 1893, and Alexander Graham Bell developed a gigantic passenger-carrying tetrahedral-celled kite from 1895 to 1910. Some of the most important full-scale model flight attempts were made by Samuel Langley, who created the first heavier-than-air, gasoline-powered engine which actually flew. The 'aerodrome', which he called it, was powered by a 53 horsepower 5-cylinder radial engine and later crashed into the Potomac river on December 1903 -- days before the Wrights' historic flight.

Throughout this century, major developments would give inventors a sound basis in experimental aerodynamics, although stability and control required for sustained flight had not been acquired. Most importantly, inventors noticed that successful, powered flight required light gasoline engines instead of the cumbersome steam engines previously used.


IV. KITTYHAWK AND AFTER

From 1903 to today, it's remarkable how far aviation has come. On December 17, 1903, at 10:35 a.m., the Wright brothers (Orville at the controls) made the first heavier-than-air, machine-powered flight which lasted 12 seconds and spanned 120 feet. Their first flight was 102 feet short of the wingspan of the C-5 Galaxy today, yet they did what every man and woman has dreamed for centuries … they flew. Yet, not all flights were victorious, on September 17, their aircraft crashed, injuring Orville and his passenger (Lieutenant Thomas E. Selfridge). Selfridge later died of a concussion and was the first person to be killed in a powered airplane. Yet the show went on and Wilbur went to France in August 1908; on December 31, 1908, he completed a 2 hour 20 minute flight which demonstrated full control over his Flyer. The Flyer was purchased on August 2 and became the first successful military airplane. It remained in service for around two years and was retired to the Smithsonian Institution where it rests today.

Well-known in the aviation field by this time, Glenn Hammond Curtiss won the first American award, the Scientific American Trophy, for an airplane flight when he flew the 'June Bug' 5090 ft (1552m) in 1 min 42.5 sec on July 4, 1908. Curtiss also went on to win the first international speed event, at about 47mph (75.6 km/h), on August 28, 1910. He also became the first American to develop and fly a seaplane -- the first successful seaplane flight having been done by Henri Fabre of France on March 28, 1910.

Before World War I, airplane design greatly improved. Pusher biplanes (two-winged airplanes with the engine and propeller behind the wing) were succeeded by tractor biplanes (two-winged airplanes with the engine and propeller in front of the wing). Monoplane designs were rare, and when World War I began, huge biplane bombers with two to four engines were developed. Airmail was also started, although it only lasted a week. The first airmail officially approved by the U.S. Post Office Department began on September 23, 1911, and the pilot (Earle Ovington) would carry the mail on his legs and tossed the bag overboard when he reached his destination. Also in 1911, the first transcontinental flight across the U.S. was completed by Calbraith P. Rodgers. His flight from New York to California took 3 days, 10 hours, and 14 minutes, and was by a Wright aircraft.


V. BEFORE WORLD WAR II

Between 1919 and 1926, some amazing progress in record breaking for aviation took place. Captain E. F. White made a nonstop flight from Chicago to New York (727 mi - 1170km) in 1919, and Lieutenant Oakley Kelly and Lieutenant John A. Macready made the first nonstop transcontinental flight from May 2 to May 3, 1923. This flight was made from Roosevelt Field, Long Island to Rockwell Field, San Diego. The first round-the-world flight was made from April 6 to September 28, 1924. Also in 1919, the first nonstop transatlantic flight was made by John William Alcock and Arthur Whitten Brown on June 14 to June 15. It took a little over 16 hours to complete and they won the "London Daily Mail" prize of $50,000.

Mail delivery also took a major turn during these years. In 1925, Congress passed the Kelly Air Mail act which authorized the Post Office Department to contract with air-transport operators. This made it possible to transport U.S. mail by air; after this, 14 domestic airmail companies were created in 1926.


VI. DURING WORLD WAR II

During World War II, aircraft became a decisive factor in warfare. The largest operator of all international airlines in operation at this time was Pan American Airways. Pan American served 46 countries and colonies linking all continents and nearly all oceans. Small aircraft production increased significantly. Before World War II only about 193,000 people were employed in the aviation industry, and during 1941 the number increased to 450,000; also, around 3,375,000 passengers were transported by 18 U.S. airlines at this time, around 1 million more than in 1940. Airmail and express cargo would also increase by around 30 percent. But by the end of World War II, a new frontier of flight would take shape, jet and rocket propelled aircraft.


VII. AFTER WORLD WAR II

After World War II and by 1947 all the basic technology needed for aviation had been developed: jet propulsion, aerodynamics, radar, etc. Civilian aircraft orders drastically increased from 6,844 in 1941 to 40,000 by the end of 1945. One of the minor military contractors was the Boeing Company who later became the largest aircraft manufacturer in the world. With all the new technologies developed by this time, airliners were larger, faster, and featured pressurized cabins. New aerodynamic designs, metals, and power plants would result in high-speed turbojet airplanes. These planes would later be able to fly supersonically and make transoceanic flights regularly.

One of the more famous record-breaking flights around this time was the Voyager, developed by Burt Rutan. The aircraft held 1,200 gallons (4500 liters) of fuel in its 17 fuel tanks. It weighed about 9,750 lb (4420 kg) at takeoff and only 1,858 lb (840kg) upon landing. The flight, maintaining an average speed of 115.8 mph (186.3 km/h), lasted 9 days, 3 minutes, 44 seconds and covered 25,012 miles (40254 km) and was completed in December 1986.