Selected major hardware components and subsystems of the shuttle orbiter are described. These include the hardware configurations, development problems and solutions, performance requirements and attainment, major hardware fabrication problems and solutions, development test objectives and implementation, and utilization of test results for hardware refinements. The subsystems selected for discussion are the space radiator, the ammonia boiler, the flash evaporator, and avionics cold plates.
Orbiter thermal control subsystem development
1978-10-01
Conference paper
No indication
English
Orbiter integrated active thermal control subsystem test
NTRS | 1980
|Shuttle Orbiter Active Thermal Control Subsystem Design and Flight Experience
SAE Technical Papers | 1991
|Orbiter S-band communications subsystem
Tema Archive | 1978
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