Combustion Wave Structure of the Ammonium Dinitramide‐Based Ionic Liquid Propellant-Reference-Cited by-同舟云学术

Combustion Wave Structure of the Ammonium Dinitramide‐Based Ionic Liquid Propellant

Published:2022-11-28 Issue:2 Volume:48 Page:
ISSN:0721-3115
Container-title:Propellants, Explosives, Pyrotechnics
language:en
Short-container-title:Propellants Explo Pyrotec

Author:

Ide Yuichiro¹^ORCID,Izato Yu‐ichiro²^ORCID,Koshi Mitsuo²,Miyake Atsumi²,Habu Hiroto³,Tokudome Shinichiro¹³

Affiliation:

1. Department of Space and Astronautical Science SOKENDAI (The Graduate University for Advanced Studies) 252-5210 Sagamihara Japan

2. Graduate School of Environment and Information Sciences Yokohama National University 240-8501 Yokohama Japan

3. The Institute of Space and Astronautical Science Japan Aerospace Exploration Agency 252-5210 Sagamihara Japan

Publisher

Wiley

Subject

General Chemical Engineering,General Chemistry

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.202200175

Reference25 articles.

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3. Combustion characteristics of a hydroxylammonium nitrate based liquid propellant. Combustion mechanism and application to thrusters

4. R. A. Spores R. Masse S. Kimbrel C. McLean GPIM AF-M315E Propulsion System 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference &Exhibit San Jose CA USA July 15–17 2013 AIAA Paper No. 2013–3849.

5. Green Propellants Based on Ammonium Dinitramide (ADN);Larsson A.;Adv. in Spacecraft Technol.,2011