Dynamic characteristic modeling and simulation of an aerospike-shaped pintle nozzle for variable thrust of a solid rocket motor-Reference-Cited by-同舟云学术

Dynamic characteristic modeling and simulation of an aerospike-shaped pintle nozzle for variable thrust of a solid rocket motor

Published:2022-12 Issue: Volume:201 Page:364-375
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Ha Dong-Sung,Kim Hong Jip

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference18 articles.

1. Status of Army Pintle Technology for Controllable Thrust Propulsion, 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;Burroughs,2001

2. Pintle Motor Challenges for Tactical Missiles, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;Ostrander,2000

3. Innovative ArianeGroup Controllable Solid Propulsion Technologies;Caubet,2019

4. Double-pulse Solid Rocket Motor Technology-Applications and Technical Solutions, 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;Naumann,2010

5. AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;Lee,2008

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