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Kühlsystem
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Transpiration and Film Cooling of Liquid Rocket Nozzles
Vuilleumier Cycle Cryogenic Refrigerator Development
Liquefaction and Storage of In-Situ Oxygen on the Surface of Mars
On the Nature of Io's Thermal Reservoir Unit
Investigation of Methods for Transpiration Cooling Liquid Rocket Chambers Final Report
Study of Potential for Motor Vehicle Fuel Economy Improvement. Truck and Bus Panel Report No. 7
Vapor-Chamber Fin Studies Quarterly Report, Sep. 1 - Nov. 30, 1965
Necap 4.1: Nasa's Energy Cost Analysis Program Engineering Manual
Large-Scale Demonstration of Liquid Hydrogen Storage with Zero Boiloff for In-Space Applications
Summary of observed results when chilling the M-1 fuel turbopump to liquid hydrogen temperature
Necap 4.1: Nasa's Energy Cost Analysis Program Engineering Flow Chart
Recent Advances in Structures for Hypersonic Flight, Part 1
Launch Pad Closeout Operations for the Mars Science Laboratory's Heat Rejection System
Evolvable Cryogenics (eCryo) Project Technology Workshop with Industry: Thermal Venting System (TVS)
Chamber Technology for Space Storable Propellants Final Report, Jun. 1964 - Sep. 1969
Exhaust Emissions Reduction for Intermittent Combustion Aircraft Engines
Nondestructive Tests of Regenerative Chambers, Appendix
Cowling and Cooling Tests of a Fleetwings Model 33 Airplane in Flight
Modeling of Gaseous Oxygen Liquefaction Inside Mars Ascent Vehicle Propellant Tank
Effect of Oil Flow to Piston on Piston-ring Sticking and Oil Consumption in a Single-cylinder Engine
Evaluation of Systems for Control of Emissions from Rocket Motors. Phase I
Surry Power Station, Units 3 and 4. License Application, Psar, Geotechnical Report
Structural Design for Aerodynamic Heating. Part II. Analytical Studies
Mitsubishi Heavy Industries Technical Review, Vol. 34, No. 3, Ser. No. 100, October 1997