Combined Rocket and Airbreathing Propulsion Systems for Space-Launch Applications
- 1 September 1998
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 14 (5), 605-612
- https://doi.org/10.2514/2.5352
Abstract
No abstract availableThis publication has 20 references indexed in Scilit:
- Energetic Fuels for Combustion ApplicationsJournal of Energy Resources Technology, 1996
- Fluid Phenomena in Scramjet Combustion SystemsAnnual Review of Fluid Mechanics, 1996
- The Strutjet engine - The overlooked option for space launchPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- The strutjet engine - Exploding the myths surrounding high speed airbreathing propulsionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- A user's primer for comparative assessments of all-rocket and rocket-based combined-cycle propulsion systems for advanced Earth-to-orbit space transport applicationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Rocket-based combined-cycle (RBCC) powered Spaceliner class vehicles can advantageously employ vertical takeoff and landing (VTOL)Published by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Computational Fluid Dynamic Modeling of Racket; Based Combined Cycle Engine FlowfieldsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1994
- Turbo/air-augmented rocket - A combined cycle propulsion systemJournal of Propulsion and Power, 1991
- Mixing-Controlled Supersonic CombustionAnnual Review of Fluid Mechanics, 1973
- Effects of thermal compression on the performance estimates of hypersonic ramjets.Journal of Spacecraft and Rockets, 1968