Environmental Control System Considerations for Supersonic Cruising Aircraft Los Angeles Div., North American Aviation, Incorporated

Format:

Conference/Event

Author/Creator:

Christensen, L. L., author.

Conference Name:

National Aeronautic Meeting and Production Forum (1965-04-12 : Washington, District of Columbia, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1965

Summary:

Weight and the thermal environment will be major considerations in designing supersonically cruising aircraft. Because of aerodynamic heating, larger capacity environmental control systems will be required. Techniques to help minimize their weight and drag are illustrated. Factors for selecting from among various environmental systems are outlined. Low air pressure and heat sink problems are causing the air-cycle to grow in weight and complexity, but air-cycle probably will be the most acceptable for the first supersonic transports. Fuel will be used extensively as a heat sink, but heat sink conservation practices will be required. Some XB-70 experience, emphasizing weight control, is included

Notes:

Vendor supplied data

Publisher Number:

650226

Access Restriction:

Restricted for use by site license