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RAKETENANTRIEB
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keywords:(RAKETENANTRIEB)
A facility for solid-propellant response measurements under pressure-driven conditions
Investigation of the piezoelectric thrust test stand for rocket engine
Nonlinear model predictive control strategy for low thrust spacecraft missions
Measurement of detonation propulsion in helium and performance calculations
Estimation of the efficiency of optimal control of an electric rocket engine with solar power supply
Missile stability using finite elements - an unconstrained variational approach
Nondestructive evaluation of naval munitions using X-ray CT
Optimization of interplanetary trajectories of space vehicles with bi-modal nuclear rocket engines
Kinetic stability and propellant performance of Green energetic materials
Vibration testing of the TE-M-604-4-IUE rocket motor (thiokol P/N E 28639-03)
Turbine-based combined cycle propulsion system integration concept design
Hybrid Carbon-Carbon Ablative Composites for Thermal Protection in Aerospace
Flow field description for the space shuttle vernier reaction control system exhaust plumes