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British Parachute Association

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In aircraft , an ejection seat or ejector seat is a system designed to rescue the pilot or other crew of an aircraft (usually military) in an emergency. In most designs, the seat is propelled out of the aircraft by an explosive charge or rocket motor , carrying the pilot with it. The concept of an ejectable escape crew capsule has also been tried (see B-58 Hustler ). Once clear of the aircraft, the ejection seat deploys a parachute . Ejection seats are common on certain types of military aircraft.

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92-546: British Skydiving is the national governing body for skydiving in the United Kingdom. British Skydiving was founded in 1960 to organise, govern and further the advancement of sport parachuting within the UK. British Skydiving aims to encourage participation in skydiving within the UK. In 2016 there were nearly 6,000 full members and around 60,000 students, and around 30 affiliated training organisations. The association

184-443: A drogue , catching air and pulling out the main parachute or the main canopy. There are two principal systems in use: the "throw-out", where the skydiver pulls a toggle attached to the top of the pilot-chute stowed in a small pocket outside the main container: and the "pull-out", where the skydiver pulls a small pad attached to the pilot-chute which is stowed inside the container. Throw-out pilot-chute pouches are usually positioned at

276-404: A vertical wind tunnel to simulate free fall has become a discipline of its own and is not only used for training but has its own competitions, teams, and figures. Ejection seat A bungee -assisted escape from an aircraft took place in 1910. In 1916, Everard Calthrop , an early inventor of parachutes , patented an ejector seat using compressed air . Compression springs installed under

368-470: A 4-man star formation, photographed by Bob Buquor. This discipline was formerly referred to in the skydiving community as Relative Work, often abbreviated to RW, Relly or Rel. Style can be considered as the sprint of parachuting. This individual discipline is played in free fall. The idea is to take maximum speed and complete a pre-designated series of maneuvers as fast and cleanly as possible (speed can exceed 400 km/h/250 mph). Jumps are filmed using

460-577: A company limited by guarantee. The association's headquarters are at Glen Parva , Leicestershire. Following the 50th anniversary of British Skydiving, an archive project was established to record and collect the history of the sport in the UK and of the Association. The association's name was changed to British Skydiving on 27 November 2019 to bring awareness of the sport to a greater audience. British Skydiving council consists of ten elected members, together with two independent directors from outside

552-466: A competitive sport , and is widely considered an extreme sport due to the risks involved. In 2018, there were 3.3 million jumps in the US. Modern militaries utilize parachuting for the deployment of airborne forces and supplies. Special operations forces commonly employ parachuting, especially free-fall parachuting, as a method of insertion. Occasionally, forest firefighters , known as " smokejumpers " in

644-578: A fashion deemed unsafe by the appointed individual. In many countries, either the local regulations or the liability-conscious prudence of the drop zone owners require that parachutists must have attained the age of majority before engaging in the sport. The first skydive performed without a parachute was by stuntman Gary Connery on 23 May 2012 at 732 m. Due to the hazardous nature of skydiving, precautions are taken to avoid parachuting injuries and death. For first-time solo-parachutists, this includes anywhere from 4 to 8 hours of ground instruction. Since

736-436: A ground-based camera (with an exceptional lens to record the performance). Performance is timed (from the start of the manoeuvre until its completion) and then judged in public at the end of the jump. Competition includes 4 qualifying rounds and a final for the top 8. Competitors jump from a height of 2200 m to 2500 m. They rush into an acceleration stage for 15 to 20 seconds and then run their series of manoeuvres benefiting to

828-619: A handful of instances, after being forced to ditch in water. The first recorded case was Lt. B. D. Macfarlane of the Royal Navy Fleet Air Arm when he successfully ejected under water using his Martin-Baker Mk.1 ejection seat after his Westland Wyvern had ditched on launch and been cut in two by the carrier on 13 October 1954. Documented evidence also exists that pilots of the US and Indian navies have also performed this feat. As of 20 June 2011 – when two Spanish Air Force pilots ejected over San Javier airport –

920-548: A higher risk factor due to the lower mobility of the jumper and the greater risk of entanglement. For this reason, these disciplines are generally practised by experienced jumpers. USPA member drop zones in the US and Canada are required to have an experienced jumper act as a "safety officer" (in Canada DSO – Drop Zone Safety Officer; in the U.S. S&TA – Safety and Training Advisor) who is responsible for dealing with jumpers who violate rules, regulations, or otherwise act in

1012-410: A higher terminal velocity than normal. In AFF, one (or sometimes two) instructor(s) are dedicated to just one student, causing this method of training to be more expensive than static line progression, where one instructor can dispatch multiple students per load, initially from a lower altitude. At a sport skydiver's deployment altitude, the individual manually deploys a small pilot-chute which acts as

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1104-411: A main parachute result in a malfunction. Ram-air parachutes typically spin uncontrollably when malfunctioning, and must be jettisoned before deploying the reserve parachute. Reserve parachutes are packed and deployed differently; they are also designed more conservatively and built and tested to more exacting standards so they are more reliable than main parachutes, but the real safety advantage comes from

1196-730: A manual release could. Whichever method is used, a spring-loaded pilot-chute then extracts the reserve parachute from the upper half of the container. World Championships are held every two years both Indoor and Outdoor in the competition disciplines Artistic Events (Freestyle and Freefly, indoor and outdoor), Canopy Formation (outdoor only), Canopy Piloting (outdoor only), Dynamic (indoor only), Formation Skydiving (indoor and outdoor), Paraski (outdoor only), Style & Accuracy Landing (outdoor only) and Wingsuit Flying (outdoor only). Continental Championships and World Cups can be held in alternate years. There are now two competitive Artistic Events, Freestyle and Freefly. Freestyle teams consist of

1288-402: A medical care facility. In the US and in most of the western world, skydivers are required to wear two parachutes. The reserve parachute must be periodically inspected and repacked (whether used or not) by a certified parachute rigger (in the US, an FAA certificated parachute rigger every 180 days). Many skydivers use an automatic activation device (AAD) that opens the reserve parachute at

1380-531: A more dangerous activity. Reputable drop zones will suspend normal operations during inclement weather. In the United States, the USPA's Basic Safety Requirements prohibit solo student skydivers from jumping in winds exceeding 14 mph while using ram-air equipment. However, maximum ground winds are unlimited for licensed skydivers. As parachuting is an aviation activity under the visual flight rules , it

1472-403: A performer and a videographer, Freefly teams have two performers and a videographer. Skysurfing is no longer a competitive event after insufficient competitors entered in two successive World Championships. The history of these events is on this Freeflying page. Often called "Classic accuracy", this is an individual or team contest performed under an open parachute. The aim is to touch down on

1564-399: A pouch (e.g., B.O.C pouch). Activation begins when the pilot-chute is thrown out. It inflates and creates drag, pulling the pin out of the closing loop and allowing the pilot-chute to pull the deployment bag from the container. The parachute lines are pulled loose from the rubber bands and extend as the canopy starts to open. A rectangular piece of fabric called the " slider " (which separates

1656-409: A predetermined altitude if it detects that the skydiver is still in free fall. Depending on the country, AADs are often mandatory for new jumpers, and/or required for all jumpers regardless of their experience level. Some skydivers wear a visual altimeter, and some use audible altimeters fitted to their helmets. Injuries and fatalities occurring under a fully functional parachute usually happen because

1748-415: A rear-mounted engine (of the twin engines powering the design) powering a pusher propeller located at the aft end of the fuselage presenting a hazard to a normal "bailout" escape—and a few late-war prototype aircraft were also fitted with ejection seats. After World War II, the need for such systems became pressing, as aircraft speeds were getting ever higher, and it was not long before the sound barrier

1840-422: A safe landing speed. Thus, prior to the introduction of zero-zero capability, ejections could only be performed above minimum altitudes and airspeeds. If the seat was to work from zero (aircraft) altitude, the seat would have to lift itself to a sufficient altitude. These early seats were fired from the aircraft with a cannon, providing the high impulse needed over the very short length on the cannon barrel within

1932-495: A solid propellant charge to eject the pilot and seat by igniting the charge inside a telescoping tube attached to the seat. As aircraft speeds increased still further, this method proved inadequate to get the pilot sufficiently clear of the airframe. Increasing the amount of propellant risked damaging the occupant's spine, so experiments with rocket propulsion began. In 1958, the Convair F-102 Delta Dagger

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2024-581: A sudden collapse (deflation) of one or more of the involved parachutes. When this occurs, the jumpers often must quickly perform emergency procedures (if there is sufficient altitude to do so) to "cut-away" (jettison) from their main canopies and deploy their reserve canopies. Canopy collisions are particularly dangerous when occurring at altitudes too low to allow the jumpers adequate time to safely jettison their main parachutes and fully deploy their reserve parachutes. Equipment failure may contribute to fatalities and injuries. Approximately one in 750 deployments of

2116-423: A target whose center is 2 cm in diameter. The target can be a deep foam mattress or an air-filled landing pad. An electronic recording pad of 32 cm in diameter is set in the middle. It measures score in 1 cm increments up to 16 cm and displays result just after landing. The first part of any competition takes place over 8 rounds. Then in the individual competition, after these 8 selective rounds,

2208-586: A test pilot. The purpose of an ejection seat is pilot survival. The pilot typically experiences an acceleration of about 12–14 g . Western seats usually impose lighter loads on the pilots; 1960s–70s era Soviet technology often goes up to 20–22  g (with SM-1 and KM-1 gunbarrel-type ejection seats). Compression fractures of vertebrae are a recurrent side effect of ejection. It was theorised early on that ejection at supersonic speeds would be unsurvivable; extensive tests, including Project Whoosh with chimpanzee test subjects, were undertaken to determine that it

2300-469: A very important part. So classic accuracy requires high adaptability to aerology and excellent steering control. It is also the most interesting discipline for spectators due to the closeness of action (a few meters) and the possibility to be practiced everywhere (sport ground, stadium, urban place...). Today, classic accuracy is the most practiced (in competition) discipline of skydiving in the world. Previously called Canopy Relative Work, or CREW for short,

2392-429: Is a fixed cord attached to a large, stable object. It is used to open parachutes automatically for paratroopers and novice parachutists . Instructor-assisted deployment (IAD) is a parachute deployment program most adequately similar to static line. The main difference is that instead of being deployed by a static line, the student's jumpmaster (who is in the plane with them) deploys the student's parachute by throwing

2484-421: Is a skydive where the participants open their parachutes very quickly after leaving the aircraft with the intention of flying in close proximity to each other. The goal is to create various formations by "docking" with other parachutists on the jump. The dock is often accomplished by placing one's feet into the lines of another person's parachute. Formations require at least 2 people, but can have many more. Due to

2576-589: Is a statistical hazard , and may be avoided by observing simple principles, including knowing upper wind speeds, the number of party members and exit groups, and having sufficient exit separation between jumpers. In 2013, 17% of all skydiving fatalities in the United States resulted from mid-air collisions. Skydiving can be practised without jumping. Vertical wind tunnels are used to practise for free fall ("indoor skydiving" or "bodyflight"), while virtual reality parachute simulators are used to practise parachute control. Beginning skydivers seeking training have

2668-487: Is also used in the T-6 Texan II and F-35 Lightning II . Through-Canopy Penetration is similar to Canopy Destruct, but a sharp spike on the top of the seat, known as the " shell tooth ", strikes the underside of the canopy and shatters it. The A-10 Thunderbolt II is equipped with canopy breakers on either side of its headrest in the event that the canopy fails to jettison. The T-6 is also equipped with such breakers if

2760-433: Is designed to safely extract upward and land its occupant from a grounded stationary position (i.e., zero altitude and zero airspeed ), specifically from aircraft cockpits. The zero-zero capability was developed to help aircrews escape upward from unrecoverable emergencies during low-altitude and/or low-speed flight, as well as ground mishaps. Parachutes require a minimum altitude for opening, to give time for deceleration to

2852-520: Is equipped with the NPP Zvezda K-36DM ejection seat and the pilot is wearing the КО-15 protective gear, they are able to eject at airspeeds from 0 to 1,400 kilometres per hour (870 mph) and altitudes of 0 to 25 km (16 mi or about 82,000 ft). The K-36DM ejection seat features drag chutes and a small shield that rises between the pilot's legs to deflect air around the pilot. Pilots have successfully ejected from underwater in

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2944-569: Is funded by membership subscriptions and has an annually elected council which controls all aspects of skydiving on behalf of the Civil Aviation Authority . Unlike many other sports which suffer from fragmented and divided governing bodies, the British Parachute Association represents most UK skydivers, and most skydivers within the UK are members of the Association. British Skydiving is constituted as

3036-495: Is generally illegal to jump in or through clouds, according to the relevant rules governing the airspace, such as FAR 105 in the US or Faldskærmsbestemmelser ( Parachuting Ordinances ) in Denmark. Jumpers and pilots of the dropping aircraft similarly bear responsibility of following the other VFR elements, in particular ensuring that the air traffic at the moment of jump does not create a hazard. A collision with another canopy

3128-581: Is of no use on or near the ground if aircraft is in level flight at the time of the ejection. Aircraft designed for low-level use sometimes have ejection seats which fire through the canopy, as waiting for the canopy to be ejected is too slow. Many aircraft types (e.g., the BAE Hawk and the Harrier line of aircraft) use Canopy Destruct systems, which have an explosive cord (MDC – Miniature Detonation Cord or FLSC – Flexible Linear Shaped Charge) embedded within

3220-487: Is often a phase of free fall (the skydiving segment), where the parachute has not yet been deployed and the body gradually accelerates to terminal velocity . In cargo parachuting, the parachute descent may begin immediately, such as a parachute- airdrop in the lower atmosphere of Earth , or it may be significantly delayed. For example, in a planetary atmosphere , where an object is descending "under parachute" following atmospheric entry from space , may occur only after

3312-489: Is similar to that of a conventional fixed-wing aircraft; however the main rotors are equipped with explosive bolts to jettison the blades moments before the seat is fired. The only commercial jetliner ever fitted with ejection seats was the Soviet Tupolev Tu-144 . However, the seats were present in the prototype only, and were only available for the crew and not the passengers. The Tu-144 that crashed at

3404-528: The Convair F-106 Delta Dart . Six pilots have ejected at speeds exceeding 700 knots (1,300 km/h; 810 mph). The highest altitude at which a Martin-Baker seat was deployed was 57,000 ft (17,400 m) (from a Canberra bomber in 1958). Following an accident on 30 July 1966 in the attempted launch of a D-21 drone , two Lockheed M-21 crew members ejected at Mach 3.25 at an altitude of 80,000 ft (24,000 m). The pilot

3496-619: The Lexan polycarbonate canopy used on the F-16. Soviet VTOL naval fighter planes such as the Yakovlev Yak-38 were equipped with ejection seats which were automatically activated during at least some part of the flight envelope. Drag Extraction is the lightest and simplest egress system available, and has been used on many experimental aircraft. Halfway between simply "bailing out" and using explosive-eject systems, Drag Extraction uses

3588-496: The United States , use parachuting as a means of rapidly inserting themselves near forest fires in especially remote or otherwise inaccessible areas. Manually exiting an aircraft and parachuting to safety has been widely used by aviators (especially military aviators and aircrew ) and passengers to escape an aircraft that could not otherwise land safely. While this method of escape is relatively rare in modern times, it

3680-401: The hypersonic entry phase and initial deceleration that occurs due to friction with the thin upper atmosphere. The first parachute jump in history was made on 22 October 1797 by Frenchman André-Jacques Garnerin above Parc Monceau , Paris. He used a silk parachute to descend approximately 3,000 feet (910 m) from a hot air balloon. Parachuting is performed as a recreational activity and

3772-576: The 186 injured in a 110,000 parachute jump study. Due to the possibility of fractures (commonly occurring on the tibia and the ankle mortise), it is recommended that parachutists wear supportive footwear. Supportive footwear prevents inward and outward ankle rolling, allowing the PLF to safely transfer impact energy through the true ankle joint, and dissipate it via the medial gastrocnemius and tibialis anterior muscles. Parachuting in poor weather, especially with thunderstorms, high winds, and dust devils can be

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3864-492: The 1990s, the average decreased to 32.3 deaths per year. Between 2000 and 2009, the average dropped to 25.8 and over the eight years after 2009, the annual average declined to 22.4 fatalities (roughly 7.5 fatalities per one million jumps). In 2017, members of one organization, the United States Parachute Association (USPA) reported 2,585 skydiving injuries sufficiently severe to require resort to

3956-592: The Advanced Concept Ejection Seat model 2 (ACES II), perform both functions as a single action. The ACES II ejection seat is used in most American-built fighters. The A-10 uses connected firing handles that activate both the canopy jettison systems, followed by the seat ejection. The F-15 has the same connected system as the A-10 seat. Both handles accomplish the same task, so pulling either one suffices. The F-16 has only one handle located between

4048-564: The French Patent Office. The design was perfected during World War II . Prior to this, the only means of escape from an incapacitated aircraft was to jump clear ("bail out"), and in many cases this was difficult due to injury, the difficulty of egress from a confined space, g forces , the airflow past the aircraft, and other factors. The first ejection seats were developed independently during World War II by Heinkel and SAAB . Early models were powered by compressed air and

4140-450: The MDC fails to detonate. In ground emergencies, a ground crewman or pilot can use a breaker knife attached to the inside of the canopy to shatter the transparency. The A-6 Intruder and EA-6B Prowler seats were capable of ejecting through the canopy, with canopy jettison a separate option if there is enough time. CD and TCP systems cannot be used with canopies made of flexible materials, such as

4232-555: The Paris Air Show in 1973 was a production model, and did not have ejection seats. The Lunar Landing Research Vehicle , (LLRV) and its successor Lunar Landing Training Vehicle (LLTV), used ejection seats. Neil Armstrong ejected on 6 May 1968, following Joe Algranti and Stuart M. Present. The only spacecraft ever flown with installed ejection seats were Vostok , Gemini , and the Space Shuttle . Early flights of

4324-470: The Space Shuttle, which used Columbia , were with a crew of two, both provided with ejector seats ( STS-1 to STS-4 ), but the seats were disabled and then removed as the crew size was increased. Columbia and Enterprise were the only two Space Shuttle orbiters fitted with ejection seats. The Buran-class orbiters were planned to be fitted with K-36RB (K-36M-11F35) seats, but as the program

4416-488: The acrylic plastic of the canopy. The MDC is initiated when the eject handle is pulled, and shatters the canopy over the seat a few milliseconds before the seat is launched. This system was developed for the Hawker Siddeley Harrier family of VTOL aircraft as ejection may be necessary while the aircraft was in the hover, and jettisoning the canopy might result in the pilot and seat striking it. This system

4508-405: The aircraft, carrying the occupant with it, by means of either an explosive charge or a rocket propulsion system. Once clear of the aircraft, the ejection seat will deploy a parachute, although some older models entrusted this step to manual activation by the seat's occupant. In the U.S. during the 1970s, the sport averaged 42.5 fatalities annually. In the 1980s, the average dropped to 34.1, and in

4600-481: The aircrew to escape at airspeeds and altitudes high enough to otherwise cause bodily harm. These seats were designed to allow the pilot to control the plane even with the clamshell closed, and the capsule would float in case of water landings. Some aircraft designs, such as the General Dynamics F-111 , do not have individual ejection seats, but instead, the entire section of the airframe containing

4692-441: The airflow past the aircraft (or spacecraft) to move the aviator out of the cockpit and away from the stricken craft on a guide rail. Some operate like a standard ejector seat, by jettisoning the canopy, then deploying a drag chute into the airflow. That chute pulls the occupant out of the aircraft, either with the seat or following release of the seat straps, who then rides off the end of a rail extending far enough out to help clear

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4784-406: The bottom of the container – the B.O.C. deployment system – but older harnesses often have leg-mounted pouches. The latter are safe for flat-flying, but often unsuitable for freestyle or head-down flying. In a typical civilian sport parachute system, the pilot-chute is connected to a line known as the "bridle", which in turn is attached to a small deployment bag that contains the folded parachute and

4876-412: The canopy suspension lines, which are stowed with rubber bands. At the bottom of the container that holds the deployment bag is a closing loop which, during packing, is fed through the grommets of the four flaps that are used to close the container. At that point, a curved pin that is attached to the bridle is inserted through the closing loop. The next step involves folding the pilot-chute and placing it in

4968-458: The cause of more than 30% of all skydiving-related injuries and deaths. Often, injuries sustained during parachute landing are caused when a single outstretched limb, such as a hand or foot, is extended separately from the rest of the body, causing it to sustain forces disproportional to the support structures within. This tendency is displayed in the accompanying chart, which shows the significantly higher proportion of wrist and ankle injuries among

5060-399: The chest) which will release the main canopy from the harness/container. Once free from the malfunctioning main canopy, the reserve canopy can be activated manually by pulling a second handle on the front left harness. Some containers are fitted with a connecting line from the main to reserve parachutes – known as a reserve static line (RSL) – which pulls open the reserve container faster than

5152-581: The close proximity of the canopies, care has to be taken by all participants to ensure the safety of the jump. It is common for a CREW jumper to carry a hook knife to use in case they become entangled in another jumper's lines. Formation Skydiving (FS) was born in California, USA during the 1960s. The first documented skydiving formation occurred over Arvin, California in March 1964 when Mitch Poteet, Don Henderson, Andy Keech and Lou Paproski successfully formed

5244-589: The crew can be ejected as a single capsule . In this system, very powerful rockets are used, and multiple large parachutes are used to bring the capsule down, in a manner similar to the Launch Escape System of the Apollo spacecraft . On landing, an airbag system is used to cushion the landing, and this also acts as a flotation device if the Crew Capsule lands in water. A zero-zero ejection seat

5336-629: The exception of the Kaman design, the pilot would still be required to parachute to the ground after reaching a safety-point for rescue. The AERCAB project was terminated in the 1970s with the end of the Vietnam War. The Kaman design, in early 1972, was the only one which was to reach the hardware stage. It came close to being tested with a special landing-gear platform attached to the AERCAB ejection seat for first-stage ground take offs and landings with

5428-649: The first aircraft to be fitted with such a system was the Heinkel He 280 prototype jet-engined fighter in 1940. One of the He 280 test pilots, Helmut Schenk, became the first person to escape from a stricken aircraft with an ejection seat on 13 January 1942 after his control surfaces iced up and became inoperative. The fighter was being used in tests of the Argus As 014 impulse jets for V-1 flying bomb development. It had its usual Heinkel HeS 8A turbojets removed, and

5520-499: The first operational military jet in late 1944 to ever feature one, the winner of the German Volksjäger "people's fighter" home defense jet fighter design competition; the lightweight Heinkel He 162 A Spatz , featured a new type of ejection seat, this time fired by an explosive cartridge. In this system, the seat rode on wheels set between two pipes running up the back of the cockpit . When lowered into position, caps at

5612-400: The following options: Tandem skydiving or tandem parachuting refers to a type of skydiving where a student skydiver is connected to an instructor via a harness. The instructor guides the student through the whole jump from exit through freefall , piloting the canopy , and landing. The student needs only minimal instruction before making a tandem jump with the instructor. A static line

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5704-553: The hazard of the T-tail . In order to make this work, the pilot was equipped with "spurs" which were attached to cables that would pull the legs inward so the pilot could be ejected. Following this development, some other egress systems began using leg retractors as a way to prevent injuries to flailing legs, and to provide a more stable center of gravity . Some models of the F-104 were equipped with upward-ejecting seats. Similarly, two of

5796-432: The jumper. During a normal deployment, a skydiver will generally experience a few seconds of intense deceleration, in the realm of 3 to 4 g, while the parachute slows the descent from 190 km/h (120 mph) to approximately 28 km/h (17 mph). If a skydiver experiences a malfunction of their main parachute which they cannot correct, they pull a "cut-away" handle on the front right-hand side of their harness (on

5888-492: The late 1960s. Three companies submitted papers for further development: A Rogallo wing design by Bell Systems; a gyrocopter design by Kaman Aircraft ; and a mini-conventional fixed wing aircraft employing a Princeton Wing (i.e. a wing made of flexible material that rolls out and then becomes rigid by means of internal struts or supports etc. deploying) by Fairchild Hiller . All three, after ejection, would be propelled by small turbojet engine developed for target drones. With

5980-503: The losses in men and aircraft in attempts to rescue them. Both services began a program titled Air Crew Escape/Rescue Capability or Aerial Escape and Rescue Capability (AERCAB) ejection seats (both terms have been used by the US military and defence industry), where after the pilot ejected, the ejection seat would fly them to a location far enough away from where they ejected to where they could safely be picked up. A Request for Proposals for concepts for AERCAB ejection seats were issued in

6072-679: The majority of parachute injuries occur upon landing (approximately 85%), the greatest emphasis within ground training is usually on the proper parachute landing fall (PLF), which seeks to orient the body so as to evenly disperse the impact through flexion of several large, insulating muscles (such as the medial gastrocnemius , tibialis anterior , rectus femoris , vastus medialis , biceps femoris , and semitendinosus), as opposed to individual bones, tendons, and ligaments which break and tear more easily. Parachutists, especially those flying smaller sport canopies, often land with dangerous amounts of kinetic energy, and for this reason, improper landings are

6164-494: The maximum of the stored speed. Those series consist of Turns and Back-Loops to achieve in a pre-designated order. The incorrect performance of the manoeuvres gives rise to penalties that are added at run time. The performance of the athlete is defined in seconds and hundredths of a second. The competitor with the lowest cumulative time is declared the winner. Notice the complete sequence is performed by leading international experts in just over 6 seconds, penalties included. Using

6256-403: The number of lives saved by Martin-Baker products was 7,402 from 93 air forces. The company runs a club called the "Ejection Tie Club" and gives survivors a unique tie and lapel pin. The total figure for all types of ejection seats is unknown, but may be considerably higher. Early models of the ejection seat were equipped with only an overhead ejection handle which doubled in function by forcing

6348-489: The parachute lines into four main groups fed through grommets in the four respective corners of the slider) slows the opening of the parachute and works its way down until the canopy is fully open and the slider is just above the head of the skydiver. The slider slows and controls the deployment of the parachute. Without a slider, the parachute would inflate fast, potentially damaging the parachute fabric and/or suspension lines, as well as causing discomfort, injury or even death of

6440-455: The parachutist can be caught in downdrafts close to the ground. Shifting winds can cause a crosswind or downwind landing which have a higher potential for injury due to the wind speed adding to the landing speed. Another risk factor is that of "canopy collisions", or collisions between two or more skydivers under fully inflated parachutes. Canopy collisions can cause the jumpers' inflated parachutes to entangle with each other, often resulting in

6532-533: The pilot chute downward and clear of the door as the student exits. Accelerated freefall (AFF) (known in Canada as progressive freefall, and in Finland as Nova (NOpeutettu VApaapudotus, a literal translation) is a method of training for skydiving, called accelerated because the progression is the fastest way to experience solo freefall, normally from 10,000 to 15,000 feet above ground level (AGL), allowing one to reach

6624-537: The pilot to assume the right posture and by having them pull a screen down to protect both their face and oxygen mask from the subsequent air blast. Martin Baker added a secondary handle in the front of the seat to allow ejection even when pilots weren't able to reach upwards because of high g-force. Later (e.g. in Martin Baker's MK9) the top handle was discarded because the lower handle had proven easier to operate and

6716-573: The pilot's knees, since the cockpit is too narrow for side-mounted handles. Non-standard egress systems include Downward Track (used for some crew positions in bomber aircraft, including the B-52 Stratofortress ), Canopy Destruct (CD) and Through-Canopy Penetration (TCP), Drag Extraction, Encapsulated Seat, and even Crew Capsule . Early models of the F-104 Starfighter were equipped with a Downward Track ejection seat due to

6808-493: The probability of an unlikely main malfunction multiplied by the even less likely probability of a reserve malfunction. This yields an even smaller probability of a double malfunction although the possibility of a main malfunction that cannot be cut away causing a reserve malfunction is a very real risk. Static line failures pose risks of towed paratroopers. Parachuting disciplines such as BASE jumping or those that involve equipment such as wingsuit flying and sky surfing have

6900-456: The seat from the aircraft, then the under-seat rocket pack fires to lift the seat to altitude. As the rockets fire for longer than the cannon, they do not require the same high forces. Zero-zero rocket seats also reduced forces on the pilot during any ejection, reducing injuries and spinal compression. The Kamov Ka-50 , which entered limited service with Russian forces in 1995, was the first production helicopter with an ejection seat. The system

6992-555: The seat were tested. The modern layout for an ejection seat was first introduced by Romanian inventor Anastase Dragomir in the late 1920s. The design featured a parachuted cell (a dischargeable chair from an aircraft or other vehicle). It was successfully tested on 25 August 1929 at the Paris-Orly Airport near Paris and in October 1929 at Băneasa , near Bucharest . Dragomir patented his "catapult-able cockpit" at

7084-451: The seat. This limited the total energy, and thus the additional height possible, as otherwise the high forces needed would crush the pilot. Modern zero-zero technology use small rockets to propel the seat upward to an adequate altitude and a small explosive charge to open the parachute canopy quickly for a successful parachute descent, so that proper deployment of the parachute no longer relies on airspeed and altitude. The seat cannon clears

7176-496: The six ejection seats on the B-52 Stratofortress fire downward, through hatch openings on the bottom of the aircraft; the downward hatches are released from the aircraft by a thruster that unlocks the hatch, while gravity and wind remove the hatch and arm the seat. The four seats on the forward upper deck (two of them, EWO and Gunner, facing the rear of the airplane) fire upwards as usual. Any such downward-firing system

7268-509: The skydiver performed unsafe maneuvers or made an error in judgement while flying their canopy, typically resulting in a high-speed impact with the ground or other hazards on the ground. One of the most common sources of injury is a low turn under a high-performance canopy and while swooping. Swooping is the advanced discipline of gliding at high-speed parallel to the ground during landing. Changing wind conditions are another risk factor. In conditions of strong winds and turbulence during hot days,

7360-504: The sport. The council is chaired by Mary Barratt. In 2015 there were 29 affiliated drop zones within British Skydiving. These include: Parachuting Parachuting and skydiving are methods of descending from a high point in an atmosphere to the ground or ocean surface with the aid of gravity, involving the control of speed during the descent using a parachute or multiple parachutes. For human skydiving, there

7452-462: The structure. In the case of the Space Shuttle, the astronauts would have ridden a long, curved rail, blown by the wind against their bodies, then deployed their chutes after free-falling to a safe altitude. Encapsulated Seat egress systems were developed for use in the B-58 Hustler and B-70 Valkyrie supersonic bombers. These seats were enclosed in an air-operated clamshell, which permitted

7544-402: The technology of helmets had advanced to also protect from the air blast. The "standard" ejection system operates in two stages. First, the entire canopy or hatch above the aviator is opened, shattered, or jettisoned, and the seat and occupant are launched through the opening. In most earlier aircraft this required two separate actions by the aviator, while later egress system designs, such as

7636-431: The top 25% jump a semi-final round. After the semi-final round, the top 50% are selected for the final round. The competitor with the lowest cumulative score is declared the winner. Competitors jump in teams of 5 maximum, exiting the aircraft at 1,000 or 1,200 meters and opening their parachutes sequentially to allow each competitor a clear approach to the target. This sport is unpredictable because weather conditions play

7728-467: The top of the seat fitted over the pipes to close them. Cartridges, basically identical to shotgun shells, were placed in the bottom of the pipes, facing upward. When fired, the gases would fill the pipes, "popping" the caps off the end, and thereby forcing the seat to ride up the pipes on its wheels and out of the aircraft. By the end of the war, the Dornier Do 335 Pfeil —primarily from it having

7820-532: Was broken. Manual escape at such speeds would be impossible. The United States Army Air Forces experimented with downward-ejecting systems operated by a spring , but it was the work of James Martin and his company Martin-Baker that proved crucial. The first live flight test of the Martin-Baker system took place on 24 July 1946, when fitter Bernard Lynch ejected from a Gloster Meteor Mk III jet. Shortly afterward, on 17 August 1946, 1st Sgt. Larry Lambert

7912-668: Was feasible. The capabilities of the NPP Zvezda K-36 were unintentionally demonstrated at the Fairford Air Show on 24 July 1993 when the pilots of two MiG-29 fighters ejected after a mid-air collision. The minimal ejection altitude for ACES II seat in inverted flight is about 140 feet (43 m) above ground level at 150 KIAS, while the Russian counterpart – K-36DM has the minimal ejection altitude from inverted flight of 100 feet (30 m) AGL. When an aircraft

8004-495: Was occasionally used in World War I by German military aviators, and utilized extensively throughout the air wars of World War II . In modern times, the most common means of escape from an aircraft in distress is via an ejection seat . Said system is usually operated by the pilot, aircrew member, or passenger by engaging an activation device manually. In most designs, this will lead to the seat being propelled out of and away from

8096-457: Was recovered successfully, but the launch control officer drowned after a water landing. Despite these records, most ejections occur at fairly low speeds and altitudes, when the pilot can see that there is no hope of regaining aircraft control before impact with the ground. Late in the Vietnam War, the U.S. Air Force and U.S. Navy became concerned about its pilots ejecting over hostile territory and those pilots either being captured or killed and

8188-457: Was the Heinkel He 219 Uhu night fighter in 1942. In Sweden, a version using compressed air was tested in 1941. A gunpowder ejection seat was developed by Bofors and tested in 1943 for the Saab 21 . The first test in the air was on a Saab 17 on 27 February 1944, and the first real use occurred by Lt. Bengt Johansson on 29 July 1946 after a mid-air collision between a J 21 and a J 22. As

8280-452: Was the first aircraft to be fitted with a rocket-propelled seat. Martin-Baker developed a similar design, using multiple rocket units feeding a single nozzle. The greater thrust from this configuration had the advantage of being able to eject the pilot to a safe height even if the aircraft was on or very near the ground. In the early 1960s, deployment of rocket-powered ejection seats designed for use at supersonic speeds began in such planes as

8372-484: Was the first live U.S. ejectee. Lynch demonstrated the ejection seat at the Daily Express Air Pageant in 1948, ejecting from a Meteor. Martin-Baker ejector seats were fitted to prototype and production aircraft from the late 1940s, and the first emergency use of such a seat occurred in 1949 during testing of the jet-powered Armstrong Whitworth A.W.52 experimental flying wing . Early seats used

8464-591: Was towed aloft from the Erprobungsstelle Rechlin central test facility of the Luftwaffe in Germany by a pair of Messerschmitt Bf 110 C tugs in a heavy snow-shower. At 7,875 ft (2,400 m), Schenk found he had no control, jettisoned his towline, and ejected. The He 280 was never put into production status. The first operational type built anywhere to provide ejection seats for the crew

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