MIL-E-19042 › Complete Document History
Engine, Rocket, Solid Propellant, 2.2 Second Duration - 11,000 Pounds Thrust (No Superseding Document)


Obsolete Revision Information:
   CANCELLATION NOTICE 1 - ENGINE, ROCKET, SOLID PROPELLA - May 24, 1982
   BASE - Engine, Rocket, Solid Propellant, 2.2 Second Duration - 11,0 - Aug. 9, 1955