Add to ORKGComponent tests and system assembly for hydrazine fuel gas distribution system of torque generator for spacecraft attitude contro
Hydrazine operated monopropellant generators are used for spacecraft rocket engines and propellant p...
Evaluation of Planetary Explorer propulsion systems of monopropellant hydrazine type for use on Venu...
Results of a program conducted to evaluate materials for construction of a space shuttle hydrazine m...
Development of warm distribution system for hydrazine fueled gas generators for spacecraft attitude ...
The design and fabrication of a flight gas generator for the space shuttle were investigated. Critic...
Dual mode hydrazine propulsion system for attitude control and maneuvering of interplanetary spacecr...
Effort was made to include as much engineering information on each component as possible, consistent...
The portable hydrazine attitude propulsion module is described that was designed and developed to su...
Ammonia fueled resistojet thrustor system for three-axis attitude control and two-direction station-...
Dual mode hydrazine system for attitude control and maneuvering propulsion of interplanetary space p...
Turboelectric, nuclear, space power conversion system using mercury Rankine cycle - SNAP
Venting system for use with cryogenic propellants to control tank pressure during zero-gravity coas
Heat balances of combined astrionic equipment and thermal conditioning subsystem of environmental co...
Design and environmental testing of thermal conditioning unit for liquid hydrogen propellant tan
Design of thermionic reactor power systems for nuclear electric propelled unmanned spacecraf
Hydrazine operated monopropellant generators are used for spacecraft rocket engines and propellant p...
Evaluation of Planetary Explorer propulsion systems of monopropellant hydrazine type for use on Venu...
Results of a program conducted to evaluate materials for construction of a space shuttle hydrazine m...
Development of warm distribution system for hydrazine fueled gas generators for spacecraft attitude ...
The design and fabrication of a flight gas generator for the space shuttle were investigated. Critic...
Dual mode hydrazine propulsion system for attitude control and maneuvering of interplanetary spacecr...
Effort was made to include as much engineering information on each component as possible, consistent...
The portable hydrazine attitude propulsion module is described that was designed and developed to su...
Ammonia fueled resistojet thrustor system for three-axis attitude control and two-direction station-...
Dual mode hydrazine system for attitude control and maneuvering propulsion of interplanetary space p...
Turboelectric, nuclear, space power conversion system using mercury Rankine cycle - SNAP
Venting system for use with cryogenic propellants to control tank pressure during zero-gravity coas
Heat balances of combined astrionic equipment and thermal conditioning subsystem of environmental co...
Design and environmental testing of thermal conditioning unit for liquid hydrogen propellant tan
Design of thermionic reactor power systems for nuclear electric propelled unmanned spacecraf
Hydrazine operated monopropellant generators are used for spacecraft rocket engines and propellant p...
Evaluation of Planetary Explorer propulsion systems of monopropellant hydrazine type for use on Venu...
Results of a program conducted to evaluate materials for construction of a space shuttle hydrazine m...