Design and Analysis of Aerospike Nozzle to Improve Thrust in Hybrid Rocket Engine

T.Karthikeyan; S.K.Aravindhkumar; J.Arun Kumar

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Design and Analysis of Aerospike Nozzle to Improve Thrust in Hybrid Rocket Engine

机译：混合火箭发动机推力增气喷管设计与分析。

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The Present Computational Analysis deal with improvement of momentum distribution of the high temperature exhaust in Rocket Engine through change in profile of aero spike nozzle. Due to change of profile we can improve thrust and mass flow rate of exhaust

机译：当前的计算分析通过改变空气尖嘴喷嘴的轮廓来改善火箭发动机中高温排气的动量分布。由于轮廓的变化，我们可以改善排气的推力和质量流率

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《International Journal of Engineering Trends and Technology》 |2016年第7期|共页
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T.Karthikeyan; S.K.Aravindhkumar; J.Arun Kumar;
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1. Design and Analysis of Aerospike Nozzle to Improve Thrust in Hybrid Rocket Engine [J] . T.Karthikeyan, S.K.Aravindhkumar, J.Arun Kumar International Journal of Engineering Trends and Technology . 2016,第7期

机译：混合火箭发动机推力增气喷管设计与分析。
2. DEVELOPMENT OF TEST FACILITIES FOR 5 KN-THRUST HYBRID ROCKET ENGINES AND A SWIRLING-OXIDIZER-FLOW-TYPE HYBRID ROCKET ENGINE FOR TECHNOLOGY DEMONSTRATION [J] . K. Kitagawa, S. Yuasa, T. Sakurai, International journal of energetic materials and chemical propulsion . 2016,第6期

机译：5 KN推力混合火箭发动机和旋流-氧化剂流式混合火箭发动机技术示范试验装置的研制。
3. Numerical and experimental investigation of throttleable hybrid rocket motor with aerospike nozzle [J] . Hui Tian, Guo Zihao, Zhu Hao, Aerospace science and technology . 2020,第Pta1期

机译：带状钳喷嘴痉挛混合火箭电动机的数值和实验研究
4. Design and Analysis of a Reusable N2O-Cooled Aerospike Nozzle for Labscale Hybrid Rocket Motor Testing [C] . Daniel J. Grieb, Patrick Lemieux, William R. Murray, AIAA/ASME/SAE/ASEE joint propulsion conference exhibit . 2012

机译：用于实验室规模混合火箭发动机测试的可重复使用的N2O冷却气雾化喷嘴的设计和分析
5. Design of an aerospike nozzle for a hybrid rocket. [D] . Gould, Cedric Oldfield. 2008

机译：混合火箭的气嘴喷嘴设计。
6. Bioinformatics analysis of single and multi-hybrid epitopes of GRA-1 GRA-4 GRA-6 and GRA-7 proteins to improve DNA vaccine design against Toxoplasma gondii [O] . Minoo Shaddel, Mansour Ebrahimi, Mohammad Reza Tabandeh 2018

机译：GRA-1GRA-4GRA-6和GRA-7蛋白的单和多杂交表位的生物信息学分析以改善针对弓形虫的DNA疫苗设计
7. Design and Analysis of a Reusable N2O-Cooled Aerospike Nozzle for Labscale Hybrid Rocket Motor Testing [O] . Daniel Grieb, Patrick Lemieux, William Murray, 2011

机译：用于Labscale混合火箭发动机试验的可重复使用N2O冷却式气动喷嘴的设计与分析
8. Performance and Thrust-to-Weight Optimization of the Dual-Expander Aerospike Nozzle Upper Stage Rocket Engine. [R] . Hall, J. N., Hartsfield, C. R., Simmons, J. R., 2012

机译：双扩张器aerospike喷嘴上级火箭发动机的性能和推力重量优化。

Design and Analysis of Aerospike Nozzle to Improve Thrust in Hybrid Rocket Engine

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