Optimum Thrust-to-Weight Ratio for Gravity-Turn Trajectories-Reference-Cited by-同舟云学术

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Optimum Thrust-to-Weight Ratio for Gravity-Turn Trajectories

Published:2000-07 Issue:4 Volume:37 Page:543-544
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Dorrington G. E.¹

Affiliation:

1. University of London, London, England E1 4NS, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/2.3600

Reference5 articles.

1. Thomson, W. T., Introduction to Space Dynamics, 2nd ed.Wiley, New York, 1962, pp.257-259.

2. Ruppe, H. O., Introduction to Astronautics, Vol.1. 1st ed.Academic, New York, 1966, pp.85-105.

3. Ball, K. J., and Osborne, G. F., Space Vehicle Dynamics, 1st ed.Oxford Univ. Press, Oxford, 1967, pp.13-15.

4. Wiesel, W. E., Spacecraft Dynamics, 1st ed.McGraw-Hill, New York, 1989, pp.207-211.

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. Launch Vehicles;Spacecraft Systems Engineering;2011-08-12

2. Semi-Analytical Formulas for Launcher Performance Evaluation;Journal of Guidance, Control, and Dynamics;2002-05

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