Ракети з точки зору аеродинаміки. Апарати, розраховані на входження в щільні шари атмосфери/Ракеты с точки зрения аэродинамики. Аппараты, рассчитанные на вход в атмосферу/Missiles in terms of aerodynamics. Entry vehicle
Документи:
- A Study of the Motion and Aerodynamic Heating of Ballistic Missiles Entering the Earth's Atmosphere at High Supersonic Speeds [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 16 p.
- A Study of the Positions and Velocities of a Space Station and a Ferry Vehicle During Rendezvous and Return [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1961. — 40 p.
- A Study Statistical Data-Adjustment and Logi Tehnidues as Applied to the Interplanetary Midcourse Guidance Problem [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1961. — 28 p.
- Boundary-Layer Similar Solutions and Correlation Equations for Laminar Heat-Transfer Distribution in Equilibrium Air at Velocities up to 41.100 Feet Per Second [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1961. — 57 p.
- Computation of Satellite Orbits by the Hansen Method as Modified by Musen [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1962. — 55 p.
- Final Report on the Tiros I Meteorological Satellite System [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1962. — 258 p.
- Hot-wire Calorimetry: Theory and Application to Lon Rocket Research [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1961. — 45 p.
- Introducere in Dinamica Rachetei [Текст] / AL. Marinescu. — Bucuresti : Editura Academiei Republicii Socialiste Romania, 1967. — 424 p.
- Jet-Boundary Corrections for Lifting Rotors Centered in Rectangular Wind Tunnels [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1960. — 62 p.
- NACA Research on Slurry Fuels [Текст] : Report / NACA. — Washington : U.S. Government Printing Office, 1958. — 24 p.
- Nearly Circular Transfer Trajectories for Desending Satellites [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1959. — 17 p.
- Parameter Study of Insertion Conditions for Lunar Missions Including Various Trajectory Considerations [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1962. — 43 p.
- Perigee Propulsion for Orbital Launch of Nuclear Rockets [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1962. — 24 p.
- Propellant Vaporization as a Design Criterion for Rocket-Engine Combustion Chambers [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1960. — 55 p.
- Study of an Automatic System for Control of the Terminal Phase of Satellite Rendezvous [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1962. — 17 p.
- The Critical Inclination Problem in Satellite Orbit Theory [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1962. — 29 p.
- Trajectories with Constant Tangential Thrust in Central Gravitation Fields [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1960. — 73 p.
- Trajectory Control for Vehicles Entering the Earth's Athmosphere at Small Flight-Path Angles [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1961. — 29 p.
- Use of an Inertia Sphere to Damp the Angular Motions of Spinning Space Vehicles [Текст] : Technical Report / NASA. — Washington : U.S. Government Printing Office, 1962. — 12 p.
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