期刊文献+

火箭的最大载荷问题(英文)

The Questions of Maximum Payload in the Rocket
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摘要 通过对多级火箭的特征速度表达式的分析,指出了(当速度式射程减小时)多级火箭的最大载荷问题与多级火箭的最宜推进剂方案的关系,从而解决了此时的多级火箭的最大载荷问题。 In this paper from analysis for the expressions of characteristic velocity for - rocket, it point out the affinity for the question of maximum payload and the best propellant plan. Thus it solves the questions of maximum payload.
出处 《青岛大学学报(自然科学版)》 CAS 2007年第4期5-9,共5页 Journal of Qingdao University(Natural Science Edition)
关键词 载荷 特征速度 多级火箭 payload characteristic velocity multi-stage rocket
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参考文献4

  • 1Zhu Miaolong. Optimization theory of step-rockets[M]. Beijing: Astronautic Publishing House, 1988.
  • 2Zhu Miaolong. Some Theoretical Problems of the Spaceflight Mechanics (2)[M]. Beijing: Science Press, 2000.
  • 3Zhu Xue-jun, Zhu Zhi-wen, Wei-min. The Regularity of the Maximum Velocity's Change for-Rocket of Parallel Type when the Effective Jet Velocity of Every Stage Increases in Order[J]. Journal of Qingdao University (Enginering & Technology Edition), 2006, 21(4): 36-43.
  • 4Zhu Xue-jun, Zhu Zhi-wen, Wei-min. The Expressions Characteristic Velocity for - Rocket of Parallel Type[M]. Journal of Qingdao University (Enginering & Technology Edition), 2007, 22 (1):76 - 81.

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