This specification defines the objectives, criteria, and configuration and establishes the requirements for performance, design, test, and qualification of the fuel subsystem for the prototype model supersonic transport airplane. This subsystem provides for the storage, distribution and management of fuel.
Supersonic Transport Development Program. Phase III Proposal. Boeing Model 2707. Fuel Subsystem Specification
1966
47 pages
Report
No indication
English
Jet & Gas Turbine Engines , Aircraft , Jet transport planes , Turbofan engines , Supersonic aircraft , Environment , Specifications , Design , Fuel tanks , Fungusproofing , Instrumentation , Venting , Control systems , Feed pumps , Jettisonable equipment , Reliability , Maintainability , Standards , Engine fuel systems components , Fuels , Transfer