Innovative Breakthroughs to a Reusable STS
Markets for fully-expendable/partially-expendable rockets including Two-Stage-To-Orbit (TSTO) and for a fully reusable human-rated Space Transportation System (STS) are discussed. Internet-related space business and in-orbit maintenance, the resupply of consumables, and the replacement of sub-systems are considered as the most important future markets for launchers. The corresponding state-of-the-art technologies of STS are reviewed, pointing out the problems. A new propulsion system, which could lead to a breakthrough for a reusable STS, is proposed.
KeywordsPropulsion System International Space Station Combine Cycle Space Shuttle Rocket Engine
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- 2.Smith, B. A.: New Launchers Seek Commercial Market Share, Aviation Week, Vol. 151, pp. 50–52, December 13, 1999Google Scholar
- 3.Kostromin, S. F.: Cost Effectiveness Estimates of the Partially Reusable Launchers Family with Uniform Components, AIAA 99-4887, presented at the 9th International Space Planes and Hypersonic Systems and Technologies Conference, Norfolk, VA, USA, November 1–5, 1990Google Scholar
- 4.Olds, J. R., et al.: Stargazer: A TSTO Bantax-X Vehicle Concept Utilizing Rocket-Based Combined-Cycle Propulsion, AIAA 99-4888, ibid.Google Scholar
- 5.Moses, P. L., et al.: An Airbreathing Launch Vehicle Design with Turbine-Based Low-Speed Propulsion and Dual Mode Scramjet High-Speed Propulsion, AIAA 99-4948, ibid.Google Scholar
- 6.Stemler, J. N., et al.: Assessment of RBCC-Powered VTHL SSTO Vehicles, AIAA 99-4947, ibid.Google Scholar
- 7.Yamanaka, T., et al.: Airbreather/Rocket Combined Cycle (ARCC) Engine for Spaceplanes, AIAA 99-4812, ibid.Google Scholar
- 8.Siebenhaar, A., et al.: The Strutjet Engine: The Overlook Option for the Space Launch, AIAA 95-3124, presented at the 31st AIAA/ASME/SAE/ASEE Joint propulsion Conference and Exhibit, San Diego, CA, USA, July 10–12,1995Google Scholar