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Analysis of Sensitivity of Parameters for Wide-Velocity-Range Reusable Flight Vehicle
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Nuo CHENG, Jun CHEN, Shun WANG, Guixuan DU
Missiles and Space Vehicles | 2026, 49(1) : 9 - 15
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Missiles and Space Vehicles | 2026, 49(1): 9-15
Launch Vehicle and Missile
Analysis of Sensitivity of Parameters for Wide-Velocity-Range Reusable Flight Vehicle
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Nuo CHENG, Jun CHEN, Shun WANG, Guixuan DU
Affiliations
  • Science and Technology on Space Physics Laboratory, Beijing, 100076
Published: 2026-02-25 doi: 10.7654/j.issn.2097-1974.20260102
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The wide-velocity-range (WVR) reusable flight vehicle, due to its extensive flight airspace and broad Mach number range, is challenging to select a fixed working state as the design point. Moreover, due to a large number of factors affecting the overall performance of the vehicle, as well as the varying impact and sensitivity of these factors in integrated air-launch system design, it has brought considerable difficulty to the integrated optimization design. A single-stage-to-orbit (SSTO) reference trajectory for the WVR reusable flight vehicle is established, conducting sensitivity analysis on key parameters from three major aspects of design: aerodynamics, propulsion, and structures. Through perturbation analysis of the reference design parameters, the impact of different parameters on the overall performance of the flight vehicle under varying operating conditions is comparatively analyzed. This successfully identifies several design parameters that significantly influence the vehicle's performance. Finally, based on the sensitivity analysis results, the study makes reasonable recommendations on subsequent optimization directions for the wide-speed-domain reusable flight vehicle from four aspects: schematic design, aerodynamics, propulsion, and structures.

WVR reusable launch vehicle  /  aerospace plane  /  single-stage-to-orbit (SSTO)  /  parameters analysis  /  parametric sensitivity analysis
Nuo CHENG, Jun CHEN, Shun WANG, Guixuan DU. Analysis of Sensitivity of Parameters for Wide-Velocity-Range Reusable Flight Vehicle[J]. Missiles and Space Vehicles, 2026 , 49 (1) : 9 -15 . DOI: 10.7654/j.issn.2097-1974.20260102
Year 2026 volume 49 Issue 1
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doi: 10.7654/j.issn.2097-1974.20260102
  • Receive Date:2025-08-14
  • Online Date:2026-03-06
  • Published:2026-02-25
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  • Received:2025-08-14
  • Revised:2026-01-14
Affiliations
    Science and Technology on Space Physics Laboratory, Beijing, 100076
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Number of
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鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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