| Development of TY-3 Microgravity Rocket System |
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| 引用本文： | YANG Jun,YE Ding you,HUANG Jian ding,YUE Fa ren (The Fourth Academy of CASC,Xi''''an 710025,China). Development of TY-3 Microgravity Rocket System[J]. 固体火箭技术, 2001, 0(4) |
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| 作者姓名： | YANG Jun YE Ding you HUANG Jian ding YUE Fa ren (The Fourth Academy of CASC Xi''''an 710025 China) |
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| 作者单位： | The Fourth Academy of CASC，Xi'an 710025，China |
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| 摘 要： | TY-3微重力火箭总长 6 0 0 0 mm,起飞质量 1 1 0 0 kg,有效载荷 5 0 kg,最大飞行高度 2 2 0 km,能提供 1 0 - 4 g约 36 0 s时间的微重力试验条件 ,该火箭已于 2 0 0 0年 1 0月飞行试验成功 ,而且一种更先进的微重力火箭系统正在设计中。
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| 关 键 词： | 探空火箭 微重力试验 TY-3微重力火箭 |
Development of TY-3 Microgravity Rocket System |
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| YANG Jun,YE Ding you,HUANG Jian ding,YUE Fa ren. Development of TY-3 Microgravity Rocket System[J]. Journal of Solid Rocket Technology, 2001, 0(4) |
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| Authors: | YANG Jun YE Ding you HUANG Jian ding YUE Fa ren |
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| Abstract: | With total length of 6000mm and launch weight of 1100kg, the TY 3 Microgravity Rocket can carry 50kg payloads to reach 220km above,and provide microgravity levels of 10 -4 g for about 360s. The rocket performed the flight test successfully on Oct. 20,2000, and a more advanced microgravity rocket system is under design. |
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| Keywords: | sounding rocket microgravity test TY 3 microgravity rocket |
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