Double-Pulse Solid Rocket Motor Technology - Applications and Technical Solutions-Reference-Cited by-同舟云学术

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Double-Pulse Solid Rocket Motor Technology - Applications and Technical Solutions

Published:2010-07-25 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Naumann Karl,Stadler Ludwig

Publisher

American Institute of Aeronautics and Astronautics

Reference15 articles.

1. Status of army pintle technology for controllable thrust propulsion

Cited by 14 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. The thermodynamic model of a solid-fuel rocket engine taking into account heat loss;JMST Advances;2024-06-25

2. SURVEY ON SELECTED RESEARCH AND DEVELOPMENT PROPULSION PROJECTS IN GERMANY DURING THE LAST 40 YEARS;International Journal of Energetic Materials and Chemical Propulsion;2024

3. Lightweight RepVGG-Based Cross-Modality Data Prediction Method for Solid Rocket Motors;Sensors;2023-11-14

4. Singular-Perturbation-based Intelligent Midcourse Guidance for Air-to-Air Missiles Equipped with Dual-Pulse Motor;2023 14th International Conference on Mechanical and Aerospace Engineering (ICMAE);2023-07-18

5. Dynamic characteristic modeling and simulation of an aerospike-shaped pintle nozzle for variable thrust of a solid rocket motor;Acta Astronautica;2022-12

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