Takeoff and landing
Vehicles that can fly can have different ways to take off and land. Conventional aircraft accelerate along the ground until sufficient lift is generated for takeoff, and reverse the process to land. Some aircraft can take off at low speed, this being a short takeoff. Some aircraft such as helicopters and Harrier Jump Jets can take off and land vertically. Rockets also usually take off vertically, but some designs can land horizontally.
- 1 Horizontal takeoff and landing
- 2 Vertical takeoff and landing
- 3 Vertical takeoff and horizontal landing
- 4 HTVL
- 5 Multi-mode configurations
- 6 References
- 7 External links
Horizontal takeoff and landing
Conventional takeoff and landing (CTOL)
Takeoff is the phase of flight in which an aircraft goes through a transition from moving along the ground (taxiing) to flying in the air, usually starting on a runway. For balloons, helicopters and some specialized fixed-wing aircraft (VTOL aircraft such as the Harrier), no runway is needed. Takeoff is the opposite of landing.
Landing is the last part of a flight, where a flying aircraft or spacecraft (or animals) returns to the ground. When the flying object returns to water, the process is called alighting, although it is commonly called "landing" and "touchdown" as well. A normal aircraft flight would include several parts of flight including taxi, takeoff, climb, cruise, descent and landing.
Short takeoff and landing (STOL)
Catapult launch and arrested recovery (CATOBAR)
CATOBAR (catapult assisted takeoff but arrested recovery) is a system used for the launch and recovery of aircraft from the deck of an aircraft carrier. Under this technique, aircraft are launched using a catapult and land on the ship (the recovery phase) using arrestor wires.
Although this system is more costly than alternative methods, it provides greater flexibility in carrier operations, since it allows the vessel to support conventional aircraft. Alternate methods of launch and recovery can only use aircraft with STOVL or STOBAR capability.
Short Take Off But Arrested Recovery (STOBAR)
STOBAR (Short Take Off But Arrested Recovery) is a system used for the launch and recovery of aircraft from the deck of an aircraft carrier, combining elements of both STOVL (Short Take-Off and Vertical Landing) and CATOBAR (Catapult Assisted Take-Off But Arrested Recovery).
Horizontal takeoff, horizontal landing (HTHL) — is the mode of operation for the first private commercial spaceplane, the two-stage-to-space Scaled Composites Tier One from the Ansari X-Prize SpaceShipOne/WhiteKnightOne combination. It is also used for the upcoming Tier 1b SpaceShipTwo/WhiteKnightTwo combination. A prominent example of its use was the North American X-15 program. In these examples the space craft are carried to altitude on a "mother ship" before launch. The failed proposals for NASA Space Shuttle replacements, Rockwell X-30 NASP used this mode of operation but were conceived as single stage to orbit.
The Lynx rocketplane is a suborbital HTHL spaceplane that was slated to begin atmospheric flight testing in late 2011, yet has not as of late 2015. Reaction Engines Skylon, a design descendant of the 1980s British HOTOL ("Horizontal Take-Off and Landing") design project, is an HTHL spaceplane currently in the early stages of development in the United Kingdom.
Both the Lynx rocketplane and SpaceShipTwo have been proffered to NASA to carry suborbital research payloads in response to NASA's suborbital reusable launch vehicle (sRLV) solicitation under the NASA Flight Operations Program.
Vertical takeoff and landing
Different terms are used for takeoff and landing depending on the source of thrust used. VTVL uses rockets, whereas VTOL uses air, propelled via some kind of rotor system.
VTOL is an acronym for vertical take-off and landing aircraft. This classification includes fixed-wing aircraft that can hover, take off and land vertically as well as helicopters and other aircraft with powered rotors, such as tiltrotors. The terminology for spacecraft and rockets is VTVL (vertical takeoff with vertical landing). Some VTOL aircraft can operate in other modes as well, such as CTOL (conventional take-off and landing), STOL (short take-off and landing), and/or STOVL (short take-off and vertical landing). Others, such as some helicopters, can only operate by VTOL, due to the aircraft lacking landing gear that can handle horizontal motion. VTOL is a subset of V/STOL (vertical and/or short take-off and landing).
Besides the ubiquitous helicopter, there are currently two types of VTOL aircraft in military service: craft using a tiltrotor, such as the Bell Boeing V-22 Osprey, and aircraft using directed jet thrust such as the Harrier family.
Vertical takeoff, vertical landing (VTVL) is a form of takeoff and landing often proposed for expendable spacecraft. Multiple VTVL rocket craft have flown.
Vertical takeoff and horizontal landing
Zero length launch system
The zero length launch system or zero length take-off system (ZLL, ZLTO, ZEL, ZELL) was a system whereby jet fighters and attack aircraft were intended to be placed upon rockets attached to mobile launch platforms. Most zero length launch experiments took place in the 1950s, during the Cold War.
VTHL—vertical takeoff, horizontal landing—is the mode of operation for all current and formerly operational orbital spaceplanes, such as the Boeing X-37, the NASA Space Shuttle, the 1988 Soviet Buran space shuttle, as well as the circa-1960 USAF Boeing X-20 Dyna-Soar project. For launch vehicles an advantage of VTHL over HTHL is that the wing can be smaller, since it only has to carry the landing weight of the vehicle, rather than the takeoff weight.
There have been several other VTHL proposals that never flew including NASA Space Shuttle proposed replacements Lockheed Martin X-33 and VentureStar. The 1990s NASA concept spaceplane, the HL-20 Personnel Launch System (HL stands for "Horizontal Lander"), was VTHL, as was a circa-2003 derivative of the HL-20, the Orbital Space Plane concept.
As of March 2011[update], two VTHL commercial spaceplanes were in various stages of proposal/development, both successors to the HL-20 design. The Sierra Nevada Corporation Dream Chaser follows the outer mold line of the earlier HL-20. The circa-2011 proposed Orbital Sciences Corporation Prometheus was a blended lifting body spaceplane that followed the outer mold line of the circa-2003 Orbital Space Plane, itself a derivative of the HL-20; however, Prometheus did not receive any NASA contracts and Orbital has announced they will not pursue further development.
German Aerospace Center studied reusable VTHL Liquid Fly-back Boosters from 1999. Design was intended to replace Ariane 5 solid rocket boosters. The U.S. government-funded, US$250,000,000, Reusable Booster System program, initiated by the USAF in 2010, had specified a high-level requirement that the design be VTHL, but the funding was discontinued after 2012.
HTVL or horizontal takeoff and vertical landing is the spaceflight equivalent of aviation HTOVL (and its subtypes CTOVL, STOVL, CATOVL). This mode of operation has not been used, but has been proposed for some systems that use a two-stage to orbit launch system with a plane based first stage, and a capsule return vehicle. One of the few HTVL concept vehicles is the 1960s concept spacecraft Hyperion SSTO, designed by Philip Bono.
Vehicles use more than one mode also exist.
Vertical/Short takeoff landing (V/STOL)
Vertical and/or short take-off and landing (V/STOL) aircraft that are able to take off or land vertically or on short runways. Vertical takeoff and landing (VTOL) includes craft that do not require runways at all. Generally, a V/STOL aircraft needs to be able to hover; helicopters are not typically considered under the V/STOL classification.
A rolling takeoff, sometimes with a ramp (ski-jump), reduces the amount of thrust required to lift an aircraft from the ground (compared with vertical takeoff), and hence increases the payload and range that can be achieved for a given thrust. For instance, the Harrier is incapable of taking off vertically with a full weapons and fuel load. Hence V/STOL aircraft generally use a runway if it is available. I.e. Short Take-Off and Vertical Landing (STOVL) or Conventional Take-off and Landing (CTOL) operation is preferred to VTOL operation.
V/STOL was developed to allow fast jets to be operated from clearings in forests, from very short runways, and from small aircraft carriers that would previously only have been able to carry helicopters.
The main advantage of V/STOL aircraft is closer basing to the enemy, which reduces response time and tanker support requirements. In the case of the Falklands War, it also permitted high performance fighter air cover and ground attack without a large aircraft carrier equipped with a catapult.
- Messier, Doug (2011-02-23). "Lynx Development Proceeds Towards First Test Flight". Parabolic Arc. Retrieved 2011-02-28.
work is coming along nicely on building the first test flight vehicle which the company hopes to fly by the end of the year.
- "Skylon FAQ". Frequently Asked Questions. Reaction Engines Limited. 2010. Retrieved 2011-02-06.
- "sRLV platforms compared". NASA. 2011-03-07. Retrieved 2011-03-10.
Lynx: Type: HTHL / Piloted ... SpaceShipTwo: Type: HTHL / Piloted
- HL-10 Lifting Body Fact Sheet, NASA, 2009-12-03, accessed 2011-02-16.
- "Vertical Takeoff & Landing Aircraft," John P. Campbell, The MacMillan Company, New York, 1962.
- Rogers 1989.
- Laskowitz, I.B. "Vertical Take-Off and Landing (VTOL) Aircraft." Annals of the New York Academy of Sciences, Vol. 107, Art.1, 25 March 1963.
- "Straight Up - A History of Vertical Flight," Steve Markman and Bill Holder, Schiffer Publishing, 2000.
- "Masten Space Systems Achieves First-Ever VTVL Midair Engine Relight Milestone on Path to Space." SpaceRef.com, 29 May 2010. Retrieved: 10 July 2011.
- AIAA 2003-09-09 Flight mechanics of manned Sub-Orbital Reusable Launch Vehicles with Recommendations for Launch and Recovery-M Sarigul-Klijn & N Sarigul-Klijn
- Orbital may wind down its commercial crew effort "Orbital may wind down its commercial crew effort" Check
|url=value (help). NewSpace Journal. 2011-04-22. Retrieved 2011-04-25.
CEO Dave Thompson said ... "I don’t, at this time, anticipate that we’ll continue to pursue our own project in that race. We’ll watch it and if an opportunity develops we may reconsider. But at this point, I would not anticipate a lot of activity on our part in the commercial crew market."
- "Liquid Fly-back Booster (LFBB)". DLR. Retrieved 9 June 2015.
- "Air Force studying reusable upper stage systems for reusable booster". RLV and Space Transport News. 2010-09-20. Retrieved 2011-03-24.
- Cogliano (2011-03-22). "Air Force launches $250M reusable booster initiative". Dayton Business Journal. Retrieved 2011-03-24.
Officials anticipate awarding up to three contracts for the project, where winners would compete for individual tasks of experiments and demonstrations that address technology, processes and other attributes of a reusable booster system, or RBS. Air Force officials envision an RBS that includes a reusable rocket and an expendable upper stage rocket. The reusable rocket would be launched vertically and return, landing aircraft style on a runway, after carrying the space craft to a point where the expendable rocket could take over.
- Ferster, Warren (2012-10-19). "Prototype Reusable Rocket Effort Felled by U.S. Budget Woes". Space News. Retrieved 2012-10-21.
- Wade, Mark. "Hyperion SSTO". Astronautix. Retrieved 2011-02-06.
The 'Hyperion' vehicle was truly remarkable since it would have been launched horizontally and landed vertically (HTVL) — an extremely rare combination. The payload capability was 110 passengers or 18t of cargo.
- "Report: F-35 Work Falls Behind Two More Years." CQ Politics, 23 July 2009