NASA has stopped developing the 274,000lb-thrust (1,220kN) J-2XD engine version for its Ares I crew launch vehicle (CLV) and will use its 294,000lb-thrust J-2X powerplant for the CLV and the Ares V cargo launch vehicle upper stages.
The liquid-oxygen, liquid-hydrogen-fuelled J-2X, named after the Apollo programme upper-stage J-2 engine, will start 133s into the flight at an altitude of 194,000ft (59,000m) and will have a mass of about 2,450kg (5,400lb). Every element of the original powerplant’s design will be altered to achieve the higher Ares launchers’ thrust needs.
To ensure the required 448s specific impulse, the engine will also use a version of the NASA/Lockheed Martin X-33 advanced technology demonstrator’s J-2S engine’s turbopump. That will be tested in October as part of the J-2X powerpack at NASA’s Stennis Space Center. Flight revealed this parallel development last year and now only the J-2X will be available from 2013. Read more