Turbojet-type engines for the airbreathing propulsion of reusable winged launchers-Reference-Cited by-同舟云学术

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Turbojet-type engines for the airbreathing propulsion of reusable winged launchers

Published:1993-01 Issue:1 Volume:29 Page:41-50
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Duparcq J.L.,Hermant E.,Scherrer D.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference5 articles.

1. Propulsion system for hypersonic transportation;Dardare,1989

2. A comparative assessment of some airbreathing engines and their integration on the STS 2000 launchers;Dufour;IAF-90-193,1990

3. Progress in airbreathing combined engines for future european launchers;Doublier,1989

4. Air breathing combined engines for space transportation systems;Lardellier;ICAS-88-1.5.2,1988

5. Etude comparative de différents systèmes de propulsion combinée;Doublier,1990

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Multi-Objective Design Optimization of Precoolers for Hypersonic Airbreathing Propulsion;Journal of Thermophysics and Heat Transfer;2017-04

2. Investigation on high angle of attack characteristics of hypersonic space vehicle;Science China Technological Sciences;2012-03-23

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