Volume 37 Issue 5
May  2022
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Article Navigation >  Journal of Aerospace Power  > 2022  >  37(5): 1054-1063
ZHANG Dongqing, LI Zhengzhou, DENG Weixin, XING Jianwen. Fast evaluation and analysis of Ma=8-10 vehicle mission performance based on vehicle and engine integration[J]. Journal of Aerospace Power, 2022, 37(5): 1054-1063. doi: 10.13224/j.cnki.jasp.20210613
Citation: ZHANG Dongqing, LI Zhengzhou, DENG Weixin, XING Jianwen. Fast evaluation and analysis of Ma=8-10 vehicle mission performance based on vehicle and engine integration[J]. Journal of Aerospace Power, 2022, 37(5): 1054-1063. doi: 10.13224/j.cnki.jasp.20210613
shu

Fast evaluation and analysis of Ma=8-10 vehicle mission performance based on vehicle and engine integration

doi: 10.13224/j.cnki.jasp.20210613

  • Aerospace Technology Institute，China Aerodynamics Research and Development Center，Mianyang Sichuan 621000，China

  • Received Date: 2021-10-26
  • Publish Date: 2022-05-28
    Abstract
  • Targeting a flight Mach number Ma=8-10 hypersonic vehicle and scramjet，an integrated performance model of vehicle and engine was built.The model can fastly evaluate the aerodynamics of vehicle，propulsion performance of engine and flight performance.The flight performances under different take-off thrust weight ratios of 0.3，0.4，0.5 and 0.6 were compared.The optimal take-off thrust weight ratio of 0.422 was obtained，with object of minimum fuel consumption，using the MATLAB optimization tools of sequence quadratic program （SQP） algorithm based on the integrated performance model of vehicle and engine.The overall parameters of the Ma=8-10 vehicle and engine conceptual scheme were given.The total mass of vehicle was 5 943 kg with the load mass of 1 000 kg.The thrust of engine was 2 505 daN.The flight time of the vehicle was 489 s with the attack angle range of 4.1° to 3.8°.The total flight distance was 1 360 km.

     

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