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Figure 1. LR 64 Rocket Engine: Minimum Time From Activation of the Squib Operated Propellant Valves to 90% of Rated Thrust Ve... |
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|  MIL-L-23822C(AS)
FIGURE 1. LR 64 ROCKET ENGINE:
MINIMUM TIME FROM ACTIVATION OF THE SQUIB OPERATED PROPELLANT VALVES
TO 90% OF RATED THRUST VERSUS TEMPERATURE
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