Injector-valve device Patent
Apparatus for cooling and injecting hypergolic propellants into combustion chamber of small rocket engine
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Apparatus for cooling and injecting hypergolic propellants into combustion chamber of small rocket engine
Inflatable honeycomb panel element for lightweight structures usable in space stations and other construction
Passive thermal control coating on aluminum foil laminate for inflatable spacecraft surfaces
Capacitor for measuring density of compressible fluid in liquid, gas, or liquid and gas phases
Landing pad assembly for aerospace vehicles
Plastic foam generator for space vehicle instrument payload package flotation in water landing
Variable thrust ion engine using thermal decomposition of solid cesium compound to produce propulsive vapor
Thermoelectric power conversion by liquid metal flowing through magnetic field
Multiple parachute system for landing control of Apollo type spacecraft
Producing high purity silicon carbide on carbon base by hydrogen reduction of silicon tetrachloride
Aircraft instrument for indicating malfunctions during takeoff
Solid state device for mapping flux and power in nuclear reactor cores
Pressure probe for sensing ambient static air pressures
Aircraft wheel spray drag alleviator for dual tandem landing gear
Spacecraft shock absorbing system for soft landings
Coupling device for linear shaped charge for space vehicle abort system
Thermal switch for transferring excess heat from one region to another heat dissipating one