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Use of Water Injection to Decrease Gasoline Consumption in an Aircraft Engine Cruising at High Power
Transfer Set DC Cabinet Temperature Investigation
Integrated Cryogenic System for Spacecraft Power, Thrust, and Cooling
Nuclear Rocket Engine Cycles. Engineering Discussion
Preliminary Service Systems Requirements for the Nrds Vehicle Test Stands
Space Electric Power Systems Study, Volume 4 Final Report, Nov. 1961 - Dec. 1962
Aec--Nasa Space Nuclear Propulsion Office X-Engine Performance Analysis
Vapor-Chamber Fin Studies First Quarterly Report, May 28 - Aug. 28, 1965
United States Department of Commerce Auto-on-Train Project Equipment Review
Preliminary Spacecraft Thermal Integration Analysis
Silent, 3.75 KW Liquid Hydrocarbon-Air Fuel Cell Powerplant. Volume II. Figures and Tables
A Solar Cell and Heater System to Reduce the Temperature Variation of Units in a Spacecraft
300-Ekw Thermionic Reactor Design Study. Final Report
Design Study (Of) Electrical Component Technology for 0.25 to 10.0 Megawatt Space Power Systems
DC Regulator for Low Pressure Mercury Lamps (Pen-Ray)
Initial Production Test of Heater, Hot Oil, Trailer Mounted, 2,100,000 BTU/HR
Propellant Feed System. S-054-012