|This article needs additional citations for verification. (March 2009)|
One of the most prominent and well-known examples of this type of aircraft was Concorde. Due to its long service in commercial airlines, Concorde has the record for the most time spent in supercruise; it has spent more time in supercruise than all other aircraft combined.
Most military aircraft use afterburners (or reheat) to travel at supersonic speeds and cannot reach supersonic speeds using the dry engine thrust. Afterburners are highly inefficient compared to conventional jet engine operation due to the low pressures typically found in the exhaust section. This limits most aircraft to using afterburners for only very short periods. Therefore, an aircraft that can supercruise has generally greater endurance at supersonic speeds than one which cannot. Supercruise capability is also an advantage for stealth aircraft, as an afterburner plume both reflects radar signals and creates a significant infrared signature.
The first turbine-powered aircraft to exceed Mach 1 in level flight without afterburners was the un-reheated Armstrong Siddeley Sapphire powered P.1 prototype of the English Electric Lightning, on August 11, 1954. Previously this aircraft, WG760, flown by Roland Beamont had unknowingly exceeded Mach 1 in the climb on its first flight on the 4th of August, 1954, although due to position error, the Mach meter had only shown a maximum of Mach 0.95, and Beamont, who had not noticed any change in behaviour of the aircraft, was surprised when informed of the fact after the flight data had been analysed. However, this early demonstration of supercruise was extremely limited; the Lightning could supercruise at approximately Mach 1.22 while later versions were able to achieve much higher speeds.
The British Aircraft Corporation Tactical Strike/Reconnaissance 2 (TSR-2), which first flew on September 27, 1964, was one of the first military aircraft specifically designed to cruise supersonically; one of the planned mission profiles was for a supersonic cruise at Mach 2.00 at 50–58,000 ft. Supersonic cruise at lower levels was at Mach 1.1 at 200 ft. The TSR-2 used Bristol Olympus engines, a later version of which would also power Concorde.
Many of the fighters listed as capable of supercruise can only marginally exceed the speed of sound without afterburners and may only be able to do so without an external weapons load.
In day-to-day operation the Tupolev Tu-144 and Concorde both used afterburners to accelerate quickly through the high-drag transonic flight regime before deactivating them to supercruise. Doing this minimized fuel use, even though afterburners are relatively inefficient. Both aircraft were capable of achieving supersonic flight without the use of afterburners; however, doing so meant that they spent much longer in the high-drag transonic flight envelope, and this made the short use of afterburners more fuel efficient over the whole flight.
The term supercruise was originally used to describe a fighter performance requirement set forth by USAF Col. John Boyd, Pierre Sprey, and Col. Everest Riccioni, proponents of the F-16 Falcon. Following the entry into production of the F-16, they began work on an improved fighter design with the ability to cruise supersonically over enemy territory for a minimum of twenty minutes. As air combat is often the result of surprise, and the speed of the combat is determined by the speed of the surprising aircraft, this would have given a supercruise-capable design a worthwhile performance advantage in many situations. The postulated fighter would have had a top speed of just over Mach 1, and a fuel fraction in excess of 40%, the minimum required to successfully meet the twenty-minute requirement. Meeting the fuel fraction requirement necessitated a very austere design with few advanced electronics. The United States Air Force showed no interest in the proposal at that time, but years later revived the term and redefined it to apply to the requirements for the Advanced Tactical Fighter, which resulted in the F-22 Raptor.
The F-22 Raptor's supercruise capabilities are touted as a major performance advantage over other fighters. Even so, supercruising uses much more fuel to travel the same distance than at subsonic speeds: The Air Force Association estimates that use of supercruise for a 100-nautical-mile (190 km) dash as part of a mission would cut the F-22's combat radius from about 600 nautical miles (1,110 km) to about 450 nautical miles (830 km). However, this is still unconfirmed as the altitude and flight profile are classified (as are most of the F-22's capabilities).
The F-22 has demonstrated supercruise speeds of at least Mach 1.7, a difference of 320 knots (593 km/h) indicated airspeed (KIAS) at 40,000 ft (12,000 m). Supercruise in militarily significant parlance is meant to imply a significant increase in effective combat speed with a full weapons load over existing types. Virtually all current and past jet fighters, prior to the F-22, cruise at approximately Mach 0.8–0.9 with a militarily significant weapons load. The F-22 represents a significant advance in cruise speed over previous types.
The key challenge in attaining supercruise is not simply attaining a high static thrust-to-weight ratio. Engine thrust and efficiency can vary greatly with speed and altitude. In order to achieve significant dry thrust at high supersonic speed, the engine (and airframe) must be built purposely with this goal in mind. Conversely, there is nothing special about being able to marginally exceed the speed of sound with a "standard" jet engine, as any supersonic engine is capable of surviving supercruise conditions, even if they may not provide enough dry power to maintain supersonic flight.
There are a few engines in production that are designed to facilitate tactically significant supercruise.
- The Pratt & Whitney F119 in combination with the F-22 Raptor
- The Snecma M88 engine in the Dassault Rafale allows it to supercruise in dry power, even with four missiles and a 1000-liter belly tank and even in the naval version; it can supercruise while carrying six air-to-air missiles (MBDA MICA).
- The EJ200 engine built by EuroJet Turbo GmbH adds the supercruise capability in the Eurofighter Typhoon, and is capable of supercruising at Mach 1.5. Typhoon pilots have stated that Mach 1.3 is attainable in combat configuration with external stores.
- The General Electric F414G in JAS 39 Gripen NG is designed for supercruise and has been shown to achieve Mach 1.2.
NPO Saturn is developing a supercruise-capable derivative of its AL-41 engine for the Sukhoi PAK FA and the Indo-Russian Sukhoi/HAL FGFA. This is yet to bear fruit, but the stop-gap AL-31 117S engine, produced by this program, seems to achieve the supercruise goal already. It was recently announced that during testing of a Su-35BM fighter equipped with these engines it was traveling in the ~M1.1–1.2 airspeed range at nominal power and was still accelerating, thus suggesting that the supercruise was possible at even higher speed. Further testing will show the extent of this possibility.
All known supercruise aircraft can only do so at considerable altitude (where the air is thinner and so offers less resistance), which restricts the use of terrain mask and so makes any non-stealth aircraft very obvious.
Aircraft designed to cruise on afterburner
Ramjets and scramjets
Ramjet and scramjet powered aircraft have to date been experimental. There have been numerous ramjet missiles, but these engines only operate at supersonic speeds and therefore would be theoretically ideal for an aircraft intended to spend long periods in supersonic flight. Due to the exotic nature of the engines, whether this would be considered "supercruise" is largely semantic.
Aircraft with supercruise
Aircraft with supercruise include:
- English Electric Lightning (first aircraft capable of supercruise)
- Saab Draken
- Lockheed Blackbird (A-12, YF-12 and SR-71)
- Tupolev Tu-128
- Tupolev Tu-144
- Tupolev Tu-160
- BAC TSR-2
- General Dynamics F-16XL
- Eurofighter Typhoon
- Dassault Rafale
- Chengdu J-10
- Gripen NG
- Lockheed Martin F-22 Raptor
- Northrop YF-23
- Sukhoi Su-35BM
- Mikoyan MiG-31
- Advanced Medium Combat Aircraft
- AIDC F-CK-1 Ching-kuo
- Zero Emission Hyper Sonic Transport
- Sukhoi/HAL FGFA
- Sukhoi PAK FA
- [dead link]
- Stealth design of airplanes / stealth aircraft
- English Electric Aircraft and their Predecessors, Stephen Ransom & Robert Fairclough, Putnam, London, 1987, (p.227)
- Austrian Eurofighter Site in German
- F-22 Raptor.com
- "Gallery of USAF Weapons", pp. 147–155. Air Force Magazine, May 2006.
- "Air defense mission for flotille F12." Fox Three, issue 8, pg. 8. Retrieved: 2011-03-30.
- Desclaux, Jacques and Jacques Serre (2003). M88 – 2 E4: Advanced New Generation Engine for Rafale Multirole Fighter. AIAA/ICAS International Air and Space Symposium and Exposition: The Next 100 Years. 14–17 July 2003, Dayton, Ohio. AIAA 2003-2610.
- "Gripen Supercruises." Gripen International, 21 January 2009.
- Frequently Asked Questions about JSF, jsf.mil, retrieved March 2011
- Tirpak, John A. (November 2012). "The F-35’s Race Against Time". airforce-magazine.com. Air Force Association. Retrieved 6 November 2012.
- Su-35BM testing report on Lenta.ru (in Russian)
- "Flying the SR-71 Blackbird" Col. Richard H. Graham, USAF (Retd), ISBN 0-7603-3239-8 p132
- Jenkins, Dennis R.; Tony R. Landis, Alvin S. White, and Fitzhugh L. Fulton (2005). Valkyrie: North American's Mach 3 Superbomber. Speciality Press. various pages. ISBN 1-58007-072-8.
- Powerplant, ConcordeSST—describes full cycle of Concorde's engine from takeoff to touchdown, including the turning off of reheat to begin supercruise at Mach 1.7.
- "A Totally Superior Product" (PDF). Gripen News: 2. June 2001.
- "Gripen Supercruises" (press release). Retrieved 2009-12-04.