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Radiation
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Transfer
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Quantitative Analysis of Heat Transfer in Engines
RADIATION FROM FLAMES - in gas turbine combustors
Re-Entry Physics. Volume III. Interaction of Vehicles in Early Re-Entry Environment. Chapters 1-5
THERMAL RADIATION CONSIDERATIONS FOR ADVANCED FLIGHT VEHICLES
OPTIMAL LOW-THRUST NEAR-CIRCULAR ORBITAL TRANSFER
Radiative Heating of Vehicles Entering the Earth's Atmosphere
OPTIMUM TWO-IMPULSE ORBITAL TRANSFER AND RENDEZVOUS BETWEEN INCLINED ELLIPTICAL ORBITS
RENDEZVOUS POSSIBILITIES WITH THE IMPULSE OF OPTIMUM TWO-IMPULSE TRANSFER SPECIAL REPORT NO. 1
Calorimeters: Heat Rate Sensors for Space Vehicle Boosters
Orbital parameters for artificial earth satellites up to 40,000 km altitude
SHOCK-LAYER RADIATION OF BLUNT BODIES TRAVELING AT LUNAR RETURN ENTRY VELOCITIES
BOILING HEAT TRANSFER IN A ZERO GRAVITY ENVIRONMENT
Optimum earth-to-mars roundtrip trajectories utilizing a low-thrust power-limited propulsion system.
Index to AGARD Publications 1952 - 1963, Supplement Number One
Geomagnetic Research by the Soviet Ship Mikhail Lomonosav: Review Article
Analytical Study of Moderator Wall Cooling of Gaseous Nuclear Rocket Engines
Summary of Base Thermal Environment Measurements on the Saturn I Block I Flight Vehicles
Future Fuels for Automotive Gas Turbines
Radiant Energy Transfer Measurements in Air
Study of Arc-Jet Propulsion Devices Final Report, 20 Nov. 1964 - 19 Dec. 1965
Environmental Research Satellites for Space Propulsion Systems Experiments
Preliminary Countdown Manual, NASA Missions, Vandenberg Air Force Base Pad 75-1-1
COOLING OF TURBINE ENGINES IN HELICOPTERS
Selected Bibliography and Abstracts of High-Temperature Optical Properties and Their Measurement
Lunar Dust Degradation Effects and Removal/Prevention Concepts. Volume 1 - Summary Final Report
A Solar Cell and Heater System to Reduce the Temperature Variation of Units in a Spacecraft
Pas Link Evaluations During Transfer Orbit
Balloon Flight Experiment for Calibration of Solar Cells
Radiation Interchange Factors Quarterly Report, 7 Jun. - 1 Sep. 1968
Pulsed Electromagnetic Gas Acceleration Semiannual Progress Report, 1 Jan. - 30 Jun. 1968
Entry Length for the Rocket Meteorological Radiation Shield
Temperature Field in a Crystal Heated by Radiation
The Thermal Mathematical Modelling of Spacecraft and the Experimental Verification
Internal Heat Losses and Alternative Configurations for a Liquid-Piston Two-Phase Heat Engine