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Thermal/Vacuum Testing of J–2X Engine
As part of the J–2X engine test program for
Ares V Earth Departure Stage (EDS) application, Glenn’s Plum
Brook Station B–2 facility will be modified to perform thermal/vacuum
ignition testing. Engine start and restart in conditions
equivalent to the Earth Departure Stage environment will be verified
in the test.
Plum Brook’s unique capability to hot fire test an engine
at simulated altitude temperatures and pressures will help validate
the J–2X engine’s ability to perform in space. The
B-2, Spacecraft Propulsion Test Facility was constructed originally
to conduct engine and stage testing. It was previously utilized
for thermal / vacuum testing of the Centaur RL-10 engine, Centaur
Upper Stage and the Delta 3 Upper Stage (shown).
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Delta 3 Upper Stage
Engine in the B-2 Facility |
Contact at NASA Glenn Research Center
Manager, Ares I Upper Stage
Engine: Claudia
M. Meyer
Space Flight Systems Directorate
/ Launch Systems Project Office
216-977-7511
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Upper stage J-2x engine |
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J-2x engine testing
in B-2 Test Facility at Plum Brook Station |
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Test Facility at PlumBrook
Station |
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