Space transportation systems with vertical start and ballistic elevation are presented. A numerical computer program for the evaluation of chemical and thermal jet propulsions is developed. Individual analysis of these propulsion systems and their combination for space transporters is performed and applied to specific aircraft performance analysis. Turborockets/ramjet systems and pure ramjet systems show advantageous transport potential. Propellant economy is 60 percent and hydrogen is the most suitable.
Analyse des Antriebs- und Einsatzpotentials Luftatmender Kombinationsantriebe fuer Ballistische Raumtransporter (Propulsion Analysis and Application Potential of Air Breathing Combined Propulsion for Ballistic Space Transporter)
1987
307 pages
Report
No indication
English
Jet & Gas Turbine Engines , Rocket Engines & Motors , Space Launch Vehicles & Support Equipment , Air start , Ascent propulsion systems , Propulsion system performance , Spacecraft propulsion , Chemical propulsion , Cost analysis , Jet propulsion , Ramjet engines , Rocket engines , Turbine engines , Turboramjet engines , Foreign technology
Werkstoffe fuer den Raumtransporter
Tema Archive | 1979
|Kommunikation fuer den Raumtransporter - Antennen fuer den Space Shuttle
Tema Archive | 1982
|TIBKAT | 1964