Synthesis of a FESTIP airbreathing TSTO space transportation system

Journal of Propulsion and Power

Volumn 17, Issue 6, 2001, Pages 1191-1198

  Grallert, H ^a  

^a AIRBUS DEFENCE AND SPACE   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

LAUNCHING; ORBITS; PERFORMANCE; PROPULSION; RAMJET ENGINES; TURBOJET ENGINES; WINGS;

DELTA WING; MACH NUMBER; SPACE TRANSPORTATION SYSTEM; TRAPEZOIDAL WING; TWO-STAGE-TO-ORBIT CONCEPT;

SPACE FLIGHT;

EID: 0035510128     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5894     Document Type: Article

References (10)

1. FESTIP system activities-Overview and status
2. The German hypersonics technology programme-Status report 1992
3. Progress in ESA winged launcher configurations studies
4. Optimal ascent trajectories for advanced launch vehicles
5. Generic derivation of a promising air-breathing TSTO space transportation system-from SÄNGER to FESTIP
6. Space shuttle-the history of developing the national space transportation system
7. RECORD project status (Russia-Europe Cooperation on Rocket Engine Demonstrator)
8. Kick-stage - a mandatory element of future reusable space transportation systems
9. Raptor gives composites a lift
10. SÄNGER and the German hypersonics technology programme - Status report 1991