MIL-E-19042 › Historical Revision Information
Engine, Rocket, Solid Propellant, 2.2 Second Duration - 11,000 Pounds Thrust
Engine, Rocket, Solid Propellant, 2.2 Second Duration - 11,000 Pounds Thrust (No Superseding Document)
To find similar documents by Federal Supply Class Code:
FSC 2845 (Rocket Engines and Components)
Document Number
MIL-E-19042
Revision Level
BASE
Status
Cancelled
Publication Date
Aug. 9, 1955