Author:
Yang Lei,Ye Zheng-Yin,Wu Jie
Funder
National Science Foundation of China
Reference30 articles.
1. 〈https://en.wikipedia.org/wiki/Air_launch_to_orbit#Advantages〉
2. S.M. Poth, M.A. Fisher, D.W. Levy, et al. Design of an airborne launch vehicle and an air launched space booster. AIAA Aircraft Design, Systems and Operations Meeting,Monterey,1993. Paper AIAA1993-3955
3. Analysis and optimization of an air-launch-to-orbit separation;Henri;Acta Astronaut.,2015
4. R.L. Thomas, D.G. Thomas, B. Morgan. Flight testing a parachute orientation system to Air-Launch rockets into low earth orbit. 19th AIAA Aerodynamic Decelerator System Technology Conference and Seminar, Williamsburg, 2007. Paper AIAA2007-2556
5. S.K. Marti, S.K. Nesrin, G. C. Hudson, et al. Selection of a carrier aircraft and a launch method for air launching space vehicles. AIAA SPACE 2008 Conference & Exposition, San Diego, 2008. Paper AIAA 2008-7835
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