Space Shuttle
Abstract
The development of the Space Shuttle is reviewed, and major design features of the initial Orbiter OV-101, now under construction, are summarized. The aerodynamic aspects of the double-delta wing platform and the short fuselage design are discussed. The thermal protection system, designed to cope with temperatures up to 2300 F, is detailed, with special attention to the quartz-based high-temperature reusable surface insulation coating the underside of the Shuttle. The upper surface of the craft is protected by a thinner low-temperature reusable surface insulation with emissivity greater than 80%; coated Nomex felt reusable insulation is used for thermal protection up to 700 F. The flight control, propulsion, and orbital manoeuvering systems are outlined, and the problem of weight control is discussed. Main design data are given for the Orbiter, Shuttle, the external H2 tank, and the solid-rocket boosters.
- Publication:
-
Flight International
- Pub Date:
- December 1975
- Bibcode:
- 1975FlInt.108..923W
- Keywords:
-
- Aerodynamic Configurations;
- Space Shuttle Orbiters;
- Spacecraft Configurations;
- Spacecraft Design;
- Aspect Ratio;
- Delta Wings;
- Orbital Maneuvers;
- Payloads;
- Propulsion System Configurations;
- Skylab Program;
- Spacelab;
- Thermal Protection;
- Weight Analysis;
- Launch Vehicles and Space Vehicles