Influence of Solid Rocket Motor Slag on the Space Debris Environment

被引：0

作者：

Bao-Jun Pang ^{[1
]}

Ke-Ke Peng ^{[1
]}

Wei-Ke Xiao ^{[2
]}

Fang-Fei Ju ^{[1
]}

Dong-Fang Wang ^{[1
]}

机构：

[1] Hypervelocity Impact Research Center,Harbin Institute of Technology

[2] Dept. Astronautical Engineering,Harbin Institute of Technology

来源：

Journal of Harbin Institute of Technology(New series) | 2013年 / 06期

关键词：

solid rocket motor; slag; space debris; orbital distribution; spatial density;

D O I：

暂无

中图分类号：

V435 [固体推进剂火箭发动机];

学科分类号：

080703 ; 082502 ;

摘要：

The resulting slag particles from solid rocket motor( SRM) firings are an important component of space debris environment. Slag sizes as large as 1 cm have been witnessed in ground tests,and comparable sizes have been also estimated via observations of sub-orbital tail-off events. We achieve slag initial data based on MASTER slag model and SRM historical launch data,and propagate slag long-term orbital evolution taking into account the zonal harmonics J2,atmospheric drag,solar radiation pressure and luni-solar attraction to discuss the slag size distribution and orbital characteristics. Finally,future slag debris environment is evaluated based on two different launch rate assumptions. The result shows that current launch frequency will make the slag population sustain growth and the population will not decrease at once even if there are no more launches in the future.

引用

页码：15 / 20

页数：6

共 50 条

[31] Possible Directions for Reducing the Influence of The Rocket and Space Industry on the Environment
Novikov, V. K.
Novikov, S. V.
Tatarinov, V. V.
XLIII ACADEMIC SPACE CONFERENCE, DEDICATED TO THE MEMORY OF ACADEMICIAN S P KOROLEV AND OTHER OUTSTANDING RUSSIAN SCIENTISTS - PIONEERS OF SPACE EXPLORATION, 2019, 2171
[32] Influence of pressure of environment on conductivity of solid rocket exhaust plume
Shi, Yan-Xiang
Ge, De-Biao
Wu, Jian
Dianbo Kexue Xuebao/Chinese Journal of Radio Science, 2008, 23 (06): : 1115 - 1118
[33] The orbital distribution and dynamics of solid rocket motor particle clouds for an implementation into the master debris model
Wegener, P
Krag, H
Rex, D
Bendisch, J
Klinkrad, H
SPACE DEBRIS, 1999, 23 (01): : 161 - 164
[34] Integrated Design Optimization for Motor and Trajectory of Near Space Solid Rocket Motor Powered Vehicle
Ren P.-F.
Wang H.-B.
Zhou G.-F.
Wang L.
Cai Q.
Han Y.-H.
Yu J.-Q.
Yuan Y.
Tuijin Jishu/Journal of Propulsion Technology, 2021, 42 (09): : 1936 - 1947
[35] Influence of dynamic lateral overload on internal ballistics of solid rocket motor
Tian Z.
Li J.
He Y.
Wang N.
Hangkong Dongli Xuebao/Journal of Aerospace Power, 2023, 38 (02): : 504 - 512
[36] SPACE-SHUTTLE REDESIGNED SOLID ROCKET MOTOR FIELD JOINT VERIFICATION
PERRY, M
EDDY, N
GRUET, L
MAW, J
JOURNAL OF PROPULSION AND POWER, 1991, 7 (02) : 139 - 145
[37] Space Shuttle Solid Rocket Motor Plume Pressure and Heat Rate Measurements
von Eckroth, Wulf
Struchen, Leah
Trovillion, Thomas
Perez, Rafael
Nerolich, Shaun
Parlier, Chris
JOURNAL OF SPACECRAFT AND ROCKETS, 2014, 51 (01) : 281 - 295
[38] Convective heat transfer in the reusable solid rocket motor of the space transportation system
Ahmad, RA
HEAT TRANSFER ENGINEERING, 2005, 26 (10) : 30 - 45
[39] Space shuttle solid rocket motor aft-end internal flows
Woodward Waesche, R.H., 1600, (05):
[40] SPACE SHUTTLE SOLID ROCKET MOTOR (SRM) FIELD JOINT: REVIEW PAPER
Gharouni, S. Mohammad
Panahiha, Hamid M.
Jam, Jafar Eskandari
METALLURGICAL & MATERIALS ENGINEERING, 2014, 20 (03) : 155 - 163

← 1 2 3 4 5 →