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Simulation Study on Pressure Holding Process of Cold Air Simulated Rocket Interstage Separation Test
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Xiaohao LI, Wuxian PAN, Guangwu LI, Hongxing ZUO, Yuchuan LUO
Missiles and Space Vehicles | 2024, 47(4) : 41 - 46
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Missiles and Space Vehicles | 2024, 47(4): 41-46
Propulsion
Simulation Study on Pressure Holding Process of Cold Air Simulated Rocket Interstage Separation Test
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Xiaohao LI, Wuxian PAN, Guangwu LI, Hongxing ZUO, Yuchuan LUO
Affiliations
  • Xi'an Aerospace Institute of Solid Propulsion Control and Measurement Technology,Xi'an,710025
Published: 2024-08-25 doi: 10.7654/j.issn.2097-1974.20240407
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Interstage thermal separation is one of the core technologies in the flight process of solid rocket. The traditional "three in one" test usually includes three main subsystems: upper stage motor, servomechanism and separation system. For practical engineering development, it is costly, expensive and long cycle. It can only be used for system level performance verification test, and is not suitable for exploratory developmental test. Based on the new ground test method of cold air simulated rocket interstage separation test, combined with theoretical model, numerical simulation and ground test verification, the internal flow field in the initial pressure holding stage of interstage separation is simulated, the law of gas pressure change in interstage section is revealed, and the test mechanism of cold air simulated rocket interstage separation is expounded; Through numerical simulation analysis, the effects of different initial pressure of pressure accumulator, different volume of pressure accumulator, different pipe area and different volume of interstage section on the change of gas pressure are studied, which provides a solution for the design of interstage separation test of cold air simulation.

cold air simulation  /  interstage separation  /  pressure holding process  /  numerical simulation  /  pressure change
Xiaohao LI, Wuxian PAN, Guangwu LI, Hongxing ZUO, Yuchuan LUO. Simulation Study on Pressure Holding Process of Cold Air Simulated Rocket Interstage Separation Test[J]. Missiles and Space Vehicles, 2024 , 47 (4) : 41 -46 . DOI: 10.7654/j.issn.2097-1974.20240407
Year 2024 volume 47 Issue 4
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Article Info
doi: 10.7654/j.issn.2097-1974.20240407
  • Receive Date:2022-08-03
  • Online Date:2025-07-04
  • Published:2024-08-25
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  • Received:2022-08-03
  • Revised:2022-12-05
Affiliations
    Xi'an Aerospace Institute of Solid Propulsion Control and Measurement Technology,Xi'an,710025
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表12种不同金属材料的力学参数

Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)

Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
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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