The Aquila launch vehicle-Reference-Cited by-同舟云学术

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The Aquila launch vehicle

Published:1992-08 Issue: Volume:28 Page:99-110
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Flittie Kirk J.,Estey Paul N.,Kniffen R.Jay

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference4 articles.

1. Hybrid Rocket Development History;Altman,1991

2. Hybrid Rocket Development at the American Rocket Company;Kniffen,1990

3. The Development of a 200,000 lbf Thrust Hybrid Rocket Booster;Kniffen;IAF-91-265,1991

4. Design of a Tridyne Pressurization System for Liquid Oxygen/Polybutadiene Hybrid Rocket Motors;Mueller,1991

Cited by 10 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. Demonstration of dual-thrust capability in hybrid rockets using multi-layered tubular fuel grains;FirePhysChem;2024-12

2. Enhancing Hybrid Rocket Engine Regression Rates: The Stepped Helix Design;Journal of Propulsion and Power;2024-09

3. Bridging the Technology Gap: Strategies for Hybrid Rocket Engines;Aerospace;2023-10-22

4. The Stepped Helix Hybrid Rocket Engine;AIAA AVIATION 2023 Forum;2023-06-08

5. Real-Time Deep Throttling Tests of a Hydrogen Peroxide Hybrid Rocket Motor;Journal of Propulsion and Power;2022-09

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