DragonFly | |
---|---|
Type | Space capsule prototype |
Class | SpaceX Dragon 2 |
Eponym | Dragonflies |
Serial no. | C201 |
Owner | SpaceX |
Manufacturer | SpaceX |
History | |
First flight |
|
Flights | 1 |
Flight time | 109 seconds |
Fate | Retired |
SpaceX Dragon 2s | |
The Dragon 2 DragonFly (Dragon C201) was a prototype suborbital rocket-powered test vehicle for a propulsively-landed version of the SpaceX Dragon 2. DragonFly underwent testing in Texas at the McGregor Rocket Test Facility in October 2015. However, the development eventually ceased as the verification burden imposed by NASA was too great to justify it.
The DragonFly test vehicle is powered by eight SuperDraco hypergolic rocket engines, arranged in a redundant pattern to support fault-tolerance in the propulsion system design. [1] SuperDracos use a storable propellant combination of monomethylhydrazine (MMH) fuel and nitrogen tetroxide oxidizer (NTO), the same propellants used in the much smaller Draco thrusters designed for attitude control and maneuvering on the first-generation Dragon spacecraft. [2] While SuperDraco engines are capable of 73,000 newtons (16,400 lbf) of thrust, during use on DragonFly flight test vehicle, each will be throttled to less than 68,170 newtons (15,325 lbf) to maintain vehicle stability. [2]
In May 2014, SpaceX publicly announced an extensive test program for a propulsively-landed space capsule called DragonFly. [3] The tests were to be run in Texas at the McGregor Rocket Test Facility in 2014–2015. [3] A flight test program of up to 60 [4] flights was proposed.
An outline for thirty of those flights included two propulsive assist (parachutes plus thrusters) and two propulsive landing (no parachutes) landing-only test flights, where DragonFly would be dropped from a helicopter at an altitude of approximately 3,000 meters (10,000 ft). The other 26 test flights were projected to be vertical takeoff, vertical landing (VTVL) test flights that will take off from a purpose-built pad: eight were to be propulsive assist hops (landing with parachutes plus thrusters) and 18 were to be full propulsive hops, where the landing is made with only rocket propulsion, similar to the Grasshopper and F9R Dev booster stage test flights that SpaceX also flew out of their McGregor facility. [2]
Test flights were planned to include a subset of tests that would test both the DragonFly space capsule and the attached trunk, an unpressurized structure that typically carries mission-specific cargo and houses the power supply system for Dragon orbital flights. The others were planned to be test landings of only the capsule itself, without the trunk. [1]
A Final Environmental Assessment was issued by the FAA in August 2014. The FAA determined that the DragonFly test program "would not significantly impact the quality of the human environment." [4] The assessment estimated that the program would take two years for SpaceX to complete and considered a total of 30 annual operations of the DragonFly test vehicle in each year of operation. [4] SpaceX received a renewal permit from the FAA on July 29, 2016, to continue another year of flight testing. [5]
The DragonFly test vehicle—formerly the Dragon2 test article that was used in the May 2015 pad abort test—was at McGregor for the start of the two-year test program by October 2015. [6] However, the development eventually ceased as the verification burden imposed by NASA was too great to justify it. [7]
Space Exploration Technologies Corp., commonly referred to as SpaceX, is an American space technology company. Since its founding in 2001, the company has made numerous advancements in rocket propulsion, reusable launch vehicle, human spaceflight and satellite constellation technology. By the late 2010s, SpaceX had become the world's dominant space launch provider, its launch cadence rivaling that of the Chinese space program and eclipsing all those of its private competitors. SpaceX, NASA and the United States Armed Forces work closely together by means of governmental contracts.
A launch escape system (LES) or launch abort system (LAS) is a crew-safety system connected to a space capsule. It is used in the event of a critical emergency to quickly separate the capsule from its launch vehicle in case of an emergency requiring the abort of the launch, such as an impending explosion. The LES is typically controlled by a combination of automatic rocket failure detection, and a manual activation for the crew commander's use. The LES may be used while the launch vehicle is on the launch pad, or during its ascent. Such systems are usually of three types:
Vertical takeoff, vertical landing (VTVL) is a form of takeoff and landing for rockets. Multiple VTVL craft have flown. A notable VTVL vehicle was the Apollo Lunar Module which delivered the first humans to the Moon. Building on the decades of development, SpaceX utilised the VTVL concept for its flagship Falcon 9 first stage, which has delivered over three hundred successful powered landings so far.
Reusable spacecraft are spacecraft capable of repeated launch, atmospheric reentry, and landing or splashdown. This contrasts with expendable spacecraft which are designed to be discarded after use, although many partially reusable spacecraft discard some kind of expendable module before reentry and recovery.
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The Falcon 9 v1.0 was the first member of the Falcon 9 launch vehicle family, designed and manufactured by SpaceX in Hawthorne, California. Development of the medium-lift launcher began in 2005, and it first flew on June 4, 2010. The Falcon 9 v1.0 then launched four Dragon cargo spacecraft: one on an orbital test flight, then one demonstration and two operational resupply missions to the International Space Station under a Commercial Resupply Services contract with NASA.
Dragon 2 is a class of partially reusable spacecraft developed, manufactured, and operated by American space company SpaceX for flights to the International Space Station (ISS) and private spaceflight missions. The spacecraft, which consists of a reusable space capsule and an expendable trunk module, has two variants: the 4-person Crew Dragon and Cargo Dragon, a replacement for the Dragon 1 cargo capsule. The spacecraft launches atop a Falcon 9 Block 5 rocket, and the capsule returns to Earth through splashdown.
SuperDraco is a hypergolic propellant rocket engine designed and built by SpaceX. It is part of the SpaceX Draco family of rocket engines. A redundant array of eight SuperDraco engines provides fault-tolerant propulsion for use as a launch escape system for the SpaceX Dragon 2, a passenger-carrying space capsule.
3D printing began to be used in production versions of spaceflight hardware in early 2014, when SpaceX first flew a flight-critical propulsion system assembly on an operational Falcon 9 flight. A number of other 3D-printed spacecraft assemblies have been ground-tested, including high-temperature, high-pressure rocket engine combustion chambers and the entire mechanical spaceframe and integral propellant tanks for a small satellite.
Raptor is a family of rocket engines developed and manufactured by SpaceX. It is the third rocket engine in history designed with a full-flow staged combustion (FFSC) fuel cycle, and the first such engine to power a vehicle in flight. The engine is powered by cryogenic liquid methane and liquid oxygen, a mixture known as methalox.
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The Commercial Crew Program (CCP) provides commercially operated crew transportation service to and from the International Space Station (ISS) under contract to NASA, conducting crew rotations between the expeditions of the International Space Station program. American space manufacturer SpaceX began providing service in 2020, using the Crew Dragon spacecraft, and NASA plans to add Boeing when its Boeing Starliner spacecraft becomes operational no earlier than 2025. NASA has contracted for six operational missions from Boeing and fourteen from SpaceX, ensuring sufficient support for ISS through 2030.
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The Crew Dragon Launch Abort System is designed to propel the SpaceX Crew Dragon spacecraft away from a failing launch vehicle. It is equipped with 8 SuperDraco engines, each capable of generating 71 kN of thrust.