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
Optimal coplanar flight between orbits
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