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First test firing of a Raptor development engine on 25 September 2016 in McGregor, Texas. Raptor is a family of methane/liquid oxygen rocket engines under development by SpaceX since the late 2000s, [2] although LH2/LOX propellant mix was originally under study when the Raptor concept development work began in 2009. [15]
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. [15] The engine is powered by cryogenic liquid methane and liquid oxygen, a combination known as methalox.
In October 2012, SpaceX publicly announced concept work on a rocket engine that would be "several times as powerful as the Merlin 1 series of engines, and won't use Merlin's RP-1 fuel". [58] They indicated that the large engine was intended for a new SpaceX rocket, using multiple of these large engines could notionally launch payload masses of ...
When stacked and fully fueled, Starship has a mass of approximately 5,000 t (11,000,000 lb), [c] a diameter of 9 m (30 ft) [17] and a height of 121.3 m (398 ft). [6] The rocket has been designed with the goal of being fully reusable to reduce launch costs; [18] it consists of the Super Heavy booster and the Starship upper stage [19] which are powered by Raptor and Raptor Vacuum engines.
SpaceX's Rocket Development and Test Facility in McGregor, Texas is a rocket engine test facility. Every rocket engine and thruster manufactured by SpaceX must pass through McGregor for rigorous final testing, ensuring their reliability and performance before being used on flight missions. [60] [61] The facility also tests various components ...
SpaceX CEO celebrated the first test firing of a full-scale, built-for-flight Raptor engine for his Starship super-rocket in the usual way tonight: by tweeting about it. "So proud of great work by ...
Reaver is an expendable rocket engine designed for use on Firefly's Alpha rocket. It produces 184 kilonewtons (41,000 lb f ) of thrust and a specific impulse of 295.6 seconds (2.899 km/s). It is powered by RP-1 and liquid oxygen as its fuel and oxidizer, respectively.
As of 2024, four full-flow staged combustion rocket engines have been tested on test stands; the Soviet storable propellant RD-270 project at Energomash in the 1960s, the US government-funded hydrolox Integrated Powerhead Demonstrator project at Aerojet Rocketdyne in the mid-2000s, [7] SpaceX's flight capable methalox Raptor engine first test ...