A wind-tunnel investigation at subsonic and low supersonic speeds of a re-entry vehicle with retractable wings /

Bibliographic Details

Main Author:	Smith, Willard G. (Author)
Format:	Government Document eBook
Language:	English
Published:	Washington : National Aeronautics and Space Administration, February 1961.
Series:	NASA technical memorandum ; X-617.
Subjects:	Aerospace vehicles. Wind tunnel tests.
Online Access:	https://purl.fdlp.gov/GPO/gpo216704