SUPERSONIC TRANSPORT PROGRAM. PHASE II-C REPORT. AIR INDUCTION SUBSYSTEM SPECIFICATION. SST BOEING MODEL 2707.
BOEING CO SEATTLE WA SUPERSONIC TRANSPORT DIV
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This specification establishes the requirements for performance, design, test and qualification of the Air Induction Subsystem. This subsystem shall provide the engine with the quantity of air demanded within the flow distortion limits of the engine. This subsystem requires a control subsystem and an anti-icing subsystem, and provides for high pressure recovery within the flow. The installation of the subsystem is defined by the Aircraft Engine Installation Subsystem Specification D6A10113-1.
- Civilian Aircraft
- Jet and Gas Turbine Engines