Performance and technological feasibility of rocket powered HTHL-SSTO with take-off assist (aerospace plane/ekranoplane)-Reference-Cited by-同舟云学术

Performance and technological feasibility of rocket powered HTHL-SSTO with take-off assist (aerospace plane/ekranoplane)

Published:1999-11 Issue:10 Volume:45 Page:629-637
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Tomita Nobuyuki,Nebylov Alexander V,Sokolov Victor V,Ohkami Yoshiaki

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference15 articles.

1. Koelle, D. E. Survey and comparison of winged launch vehicle options, ISTS 94-g-11 V 1994

2. Bekey, I. Why SSTO rocket launch vehicles are now feasible and practical, IAF-94-V.1.524 1994

3. Berry, E. Life-cycle cost comparison of reusable launch systems, IAA-95-IAA.1.1.02 1995

4. Berry, W. and Grallert, H. Performance and technical feasibility comparison of reusable launch systems, a synthesis of the ESA winged launcher studies, IAF-95-V3.03 1995

5. Martin, A. Effects of tri-propellant engines on earth-to-orbit vehicles, AIAA-83-1187 1977

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