Optimal vertical ascent to GEO with thrust acceleration and dynamic pressure constraints-Reference-Cited by-同舟云学术

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Optimal vertical ascent to GEO with thrust acceleration and dynamic pressure constraints

Published:1995-01 Issue:1 Volume:35 Page:9-18
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Chern Jeng-Shing,Hong Zuu-Chang,Cheng Wu-Lang

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference8 articles.

1. Vertical ascent to geosynchronous orbit;Martin;J. Guidance Control Dynamics,1984

2. Pulsed laser propulsion for low cost, high volume launch to orbit;Kare,1989

3. Optimal trajectory for vertical ascent to geosynchronous Earth orbit;Chern;IAF-91-341,1991

4. Optimal ascent to GEO using laser propulsion system;Chern;IAF-92-0017,1992

5. Concepts and status of laser-supported rocket propulsion;Glumb;J. Spacecraft,1984

Cited by 3 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. Enhancing payload capacity to low earth orbit via a relay solution trajectory with laser-powered vehicles;Geo-spatial Information Science;2024-07-17

2. Overall payload ratio of a combined laser and chemical propulsion system for geo launch;Acta Astronautica;2002-04

3. Vertical Ascent to Geosynchronous Orbit with Constrained Thrust Angle;Journal of Spacecraft and Rockets;2000-01

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