Wind tunnel investigation of the supersonic stage separation aerodynamics of a generic 0.0175- scale bimese two-stage-to-orbit reusable launch vehicle configuration /

Bibliographic Details

Main Author:	Erickson, Gary E. (Author)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, April 2020.
Series:	NASA technical memorandum ; 2020-220582.
Subjects:	Supersonics. Wind tunnels. Shock waves. Boundary layer separation. Stage separation.
Online Access:	https://purl.fdlp.gov/GPO/gpo138450