Optimal nozzle Mach number for maximizing altitude of sounding rocket
Author:
Funder
University of Ulsan
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference13 articles.
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2. Drag-law effects in the Goddard problem;Tsiotras;Automatica,1991
3. Goddard problem in presence of a dynamic pressure limit;Seywald;J. Guid. Control Dyn.,1993
4. Solving the Goddard problem with thrust and dynamic pressure constraints using saturation functions;Graichen;IFAC Proc.,2008
5. Analytic approach to determine optimal conditions for maximizing altitude of sounding rocket;Lee;Aerosp. Sci. Technol.,2015
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. A self-adaptive local diversity-preserving NSGA-II for the multidisciplinary design optimization of a miniaturized supersonic rocket;Aerospace Science and Technology;2023-05
2. Optimal Thrust Programming for Two-Stage Sounding Rocket;Journal of Spacecraft and Rockets;2019-07
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