Back to Search
Start Over
Aerodynamic characteristics of a family of multistage missiles at a mach number of 6.0
- Publication Year :
- 1965
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1965.
-
Abstract
- Wind tunnel investigation of aerodynamic characteristics of cone-cylinder-flare multistage missile configurations at supersonic speed
- Subjects :
- Aerodynamics
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Publication Type :
- Report
- Accession number :
- edsnas.19650017042
- Document Type :
- Report