Performance and technical feasibility comparison of reusable launch systems: A synthesis of the ESA winged launcher studies-Reference-Cited by-同舟云学术

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Performance and technical feasibility comparison of reusable launch systems: A synthesis of the ESA winged launcher studies

Published:1996-02 Issue:4-8 Volume:38 Page:333-347
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Berry W.,Grallert H.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference5 articles.

1. Life-Cycle Cost Comparison of Reusable Launch Systems;Berry;Paper IAA-95-IAA.1.1.02,1995

2. An Investigation of Future European Winged Launcher Concepts;Grallert;IAF Paper 89-216,1989

3. Progress in ESA Winged Launcher Configuration Studies;Grallert;IAF Paper 91-199,1991

4. Studies on a Scramjet-Propelled, Horizontal Launch and Landing, Single-Stage-To-Orbit Launcher;Weinreich;AIAA Paper 93-5053,1993

5. Winged Launcher Configuration Study: Synthesis Report for Study Phases 1 to 6;Grallert;DASA FESTIP Interim Report FSS-DRI-SC-2310-001,1995

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