Development of a University-Based Simplified H₂O₂/PE Hybrid Sounding Rocket at KAIST-Reference-Cited by-同舟云学术

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Development of a University-Based Simplified H₂O₂/PE Hybrid Sounding Rocket at KAIST

Published:2017-09-30 Issue:3 Volume:18 Page:512-521
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:IJASS

Author:

Huh Jeongmoo,Ahn Byeonguk,Kim Youngil,Song Hyunki,Yoon Hosung,Kwon Sejin

Publisher

The Korean Society for Aeronautical & Space Sciences

Cited by 17 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Measurement of fuel port pressure distribution by exposed solid fuel hydrogen peroxide catalytic decomposition hybrid thruster;Acta Astronautica;2024-06

2. Hypergolic Propellants Based on High-Test Hydrogen Peroxide and Organic Compounds;Russian Journal of Applied Chemistry;2023-10

3. A practical design approach for a single-stage sounding rocket to reach a target altitude;The Aeronautical Journal;2022-03-03

4. Demonstration of tethered hovering flight of HTTP-3AT hybrid rocket;Acta Astronautica;2022-02

5. Throat length effect on the flow patterns in off-design conical nozzles;FME Transactions;2022

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