用户登录 购物车
图书馆订购 Guest
主页 旧刊 有关人员 未来大会

ISSN 在线: 2688-7231

ISBN 在线: 978-1-56700-524-0

Proceedings of the 26thNational and 4th International ISHMT-ASTFE Heat and Mass Transfer Conference December 17-20, 2021, IIT Madras, Chennai-600036, Tamil Nadu, India
December, 17-20, 2021, IIT Madras, Chennai, India

Lab level testing and ballistic performance analysis of a LO2/HTPB+20%Al hybrid motor configuration

Get access DOI: 10.1615/IHMTC-2021.230
pages 153-159

摘要

Hybrid rocket propulsion can be a viable solution for safe, high performance thrusters; as demanded by present day micro/nano satellite launchers. Among various hybrid propellant combinations, LO2/HTPB+20%Al hybrid propellant combination offer a safe, high performance, low cost and scalable solution. In this study, lab level tests carried out with LO2/HTPB+20%Al hybrid propellant combination is reported. The tests were conducted to study and improve the ignition and combustion characteristics of the motor. The ballistic performance of the hybrid motor is analyzed in depth. Potential improvements in test methodology and directions of future research are discussed.
主页 旧刊 有关人员 未来大会 中文 English Русский Português 帮助 联系我们 返回至ISHMT