Email RIS file
Bookmark
Report an Issue

Aerodynamic heating at Mach 8 of attached inflatable decelerator configurations

Author
Miserentino, R.
Published
Oct 1, 1971.
Physical Description
1 electronic document
Additional Creators
Creel, T. R., Jr.
Online Version

Availability

I Want It
I Want It

Finding items...

Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Mach 8 variable-density tunnel used for determination of aerodynamic heating of attached inflatable decelerator configurations
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19710029282.
Accession ID: 71N38758.
L-7864.
NASA-TM-X-2355.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15948291