Automatically deploying nozzle exit cone extension Patent
Automatically deploying nozzle exit cone extension
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Automatically deploying nozzle exit cone extension
Transient heat transfer gage for measuring total radiant intensity from far ultraviolet and ionized high temperature gases
Attitude detection system using stellar references for three-axis control and spin stabilized spacecraft
Method for testing rocket nozzles at high tensile stress levels
High strength, corrosion resistant cobalt-based alloys for aerospace structures
Constructing fluid spike nozzle to eliminate heat transfer and high temperature problems inherent in physical spikes
Method and apparatus for measuring potentials in plasmas
Method for shaping regeneratively cooled rocket motor casing having minimum thickness at each channel cross section
Regeneratively cooled rocket motor casing with tapered channels to insure minimum thicknesses at each channel cross section for necessary strength requirements
Propellant injection assembly having individually removable and replaceable nozzles for liquid fueled rocket engines
Electron bombardment ion rocket engine with improved propellant introduction system
Design and characteristics of linkage to alleviate rocket vehicle divergence during launch
Vibration damping system operating in low vacuum environment for spacecraft mechanisms
Variable geometry manned orbital vehicle having high aerodynamic efficiency over wide speed range and incorporating auxiliary pivotal wings
Describing assembly for opening stabilizing and decelerating flaps of flight capsules used in space research
Spin phase synchronization of cartwheel satellite in polar orbit
Payload/spent rocket engine case separation system