Stennis Space Center Site Index
J-2 Engine Gallery


Detail of the pneumatic interface to the stage at the forward end of the engine.

These lines include fuel and oxidizer tank pressurization lines; start tank fill, drain, vent, and relief lines; turbopump and thrust chamber jacket purges; and a helium tank fill line.

J-2 Engine start tank and customer connect fluid system (pneumatic interface to the stage) at Stennis Space Center
Time picture taken Tue Jun 14 11:19:46 2005
Location picture taken Rocket Park
Visitor Center
Stennis Space Center, MS
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