Materials Applications and Structural Concepts for Hypersonic Air-Induction Systems Lockheed Missiles and Space Company

Format:

Conference/Event

Author/Creator:

Paul Plank, P., author.

Conference Name:

Aeronautic and Space Engineering and Manufacturing Meeting (1969-10-06 : Los Angeles, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1969

Summary:

AbstractTypical Mach 6 hypersonic cruise vehicle data are used to define temperature, loads, and criteria, and to identify potential materials and structural concepts for air-induction systems associated with a two-dimensional variable-geometry inlet. It was found that the superalloys can be used at temperatures below 1600 F for 500 hr of life to satisfy the requirements of all air-induction system areas, by cooling with liquid hydrogen. The thermostructural concepts found to be most attractive for use in inlet designs are radiation-cooled surface panels with an insulated substructure and regeneratively-cooled plates over surface panel structures supported by an insulated substructure

Notes:

Vendor supplied data

Publisher Number:

690664

Access Restriction:

Restricted for use by site license