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Kühlsystem
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Wind Tunnel Investigation of Rear Underslung Fuselage Ducts
Use of water injection to decrease gasoline consumption in an aircraft engine cruising at high power
Transpiration and Film Cooling of Liquid Rocket Nozzles
The effect of valve clearance on knock-limited performance and engine cooling
The effect of oil consumption and piston cooling on knock-limited aircraft-engine performance
The effect of cooling-air blowers on thrust power
The Edison Infrared Space Observatory and the Study of Extra-Solar Planetary Meterial
The Development of an Airborne Information Management System for Flight Test
Tests of Several Model Nacelle-propeller Arrangements in Front of a Wing
Supercooling of thermoelectric device using a current pulse
Summary of observed results when chilling the M-1 fuel turbopump to liquid hydrogen temperature
STUDY OF CHAMBER COOLING TECHNIQUES FOR SPACECRAFT ENGINES. MONTHLY LETTER
Structural Heat Intercept, Insulation and Vibration Evaluation Rig (SHIIVER)
Spacecraft temperature control by thermostatic fins Progress report, 1 Jun. - 30 Nov. 1965
Spacecraft engine thrust chamber cooling final report, 13 may 1963 - 12 apr. 1964
Solid-state power generation and cooling micro/nanodevices for distributed system architectures
SELECTING A THRUST CHAMBER COOLING TECHNIQUE FOR SPACECRAFT ROCKET ENGINES
SELECTING A THRUST CHAMBER COOLING TECHNIQUE FOR SPACECRAFT ROCKET ENGINES
Review of flight tests of NACA C and D cowlings on the XP-42 airplane
[Research on a Self-Temperature Regulating Spacecraft Skin System]
Progress Report on the Development of Protected Construction for Hypersonic Vehicles
Program for sea level test firing of rocket engines final report, 1 sep. 1964 - 1 feb. 1965
On the Nature of Io's Thermal Reservoir Unit
Nitrous oxide supercharging of an aircraft-engine cylinder
Micro/nano spacecraft thermal control using MEMS-based pumped liquid cooling system
MEMS based pumped liquid cooling systems for micro/nano spacecraft thermal control
Measurement of Magnetostriction Between 4.2 and 77K
Mars Pathfinder mechanically pumped cooling loop
Long Term Life Testing of a Mechanically Pumped Cooling Loop for Spacecraft Thermal Control
Localized overheating in Aerobee regeneratively cooled thrust chambers
Launch Pad Closeout Operations for the Mars Science Laboratory's Heat Rejection System
Investigation of cooling problems at high chamber pressures final report, 1 jul. 1963 - 31 mar. 1965