History of U.S. Navy ramjet, scramjet, and mixed-cycle propulsion development

Journal of Propulsion and Power

Volumn 18, Issue 1, 2002, Pages 14-27

  Waltrup, P J ^a   White, M E ^a   Zarlingo, F ^a   Gravlin, E S ^a  

^a JOHNS HOPKINS UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ORDNANCE; ROCKET ENGINES; SUBSONIC AERODYNAMICS; SUPERSONIC AIRCRAFT;

WEAPON SYSTEM;

RAMJET ENGINES;

EID: 0036152955     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5928     Document Type: Article

References (19)

1. Hydrocarbon-fueled scramjet combustor investigation
2. Evolution of ramjet missile propulsion in the united states and where we are headed
3. The Talos missile
4. The beginning of hypersonic ramjet research at APL
5. Typhon - A weapon ahead of its time
6. Airbreathing propulsion for defense of the surface fleet
7. The solid-fuel ramjet
8. Solid-fuel ramjet developments by U.S. Naval Ordnance Tests Station, China Lake, California
9. Final report on development of solid fuel for ramjet sustainer motor
10. Design and performance of an integral ramjet/rocket
11. Ramjet research payoffs believed near
12. Low Mach number, connected pipe tests of a supersonic combustion ramjet missile (SCRAM) combustor and fuels
13. Summary report of connected-pipe SCRAM tests
14. SCRAM: A supersonic combustion ramjet missile
15. The national aerospace plane program: A revolutionary concept
16. The national aerospace plane program and the APL role