Overview of Hybrid Sounding Rocket Program-Reference-Cited by-同舟云学术

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Overview of Hybrid Sounding Rocket Program

Published:1997-07-06 Issue: Volume: Page:
ISSN:
Container-title:33rd Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Arves J.¹,Jones H.¹,Kline K.²,Smith K.²,Slack Ted²,Bales T.²,Arves J.¹,Jones H.¹,Kline K.²,Smith K.²,Slack Ted²,Bales T.²

Affiliation:

1. Lockheed Martin Manned Space Systems, New Orleans, LA

2. Environmental Aerosciences Corp., Miami, FL

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2799

Reference3 articles.

1. Development of a N2O/HTPB hybrid rocket motor

2. A standardized technique for evaluating hybrid rocket motor performance

Cited by 5 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. A practical design approach for a single-stage sounding rocket to reach a target altitude;The Aeronautical Journal;2022-03-03

2. Development and Test Flight of The Atlantis I Nitrous Oxide/Paraffin-based Hybrid Rocket;AIAA Propulsion and Energy 2019 Forum;2019-08-16

3. Development and Testing of a 4.4-kN Paraffin-based Hybrid Rocket Motor and Test Facility;2018 Joint Propulsion Conference;2018-07-08

4. Overview of a 4-inch OD Paraffin-Based Hybrid Sounding Rocket Program;40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2004-06-21

5. Development of a N2O/HTPB hybrid rocket motor;33rd Joint Propulsion Conference and Exhibit;1997-07-06

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