Insulation-Radiation Temperature Control of Inflatable Hypersonic Vehicles Goodyear Aircraft Corporation

Format:

Conference/Event

Author/Creator:

Ginter, R. L., author.

Conference Name:

National Aerospace Engineering & Manufacturing Meeting

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1962

Summary:

This paper presents the theory of an insulation-radiation cooling method applicable to expandable hypersonic vehicles; two simple configurations, a sphere and a cylinder, are analyzed to illustrate this method. Use of internal radiation and thin layers of insulation can reduce hot spot temperatures by as much as 33% compared to a 12% reduction possible by the use of internal radiation alone

Notes:

Vendor supplied data

Publisher Number:

620331

Access Restriction:

Restricted for use by site license