Combustion behavior of NMP-001, a nitromethane-based green rocket propellant
-
Published:2024-10
Issue:
Volume:223
Page:1-14
-
ISSN:0094-5765
-
Container-title:Acta Astronautica
-
language:en
-
Short-container-title:Acta Astronautica
Author:
Kurilov MaximORCID,
Werling LukasORCID,
Kirchberger Christoph,
Ciezki Helmut,
Schlechtriem Stefan
Reference64 articles.
1. Substance infocard - hydrazine;European Chemicals Agency,2024
2. W.M. Marshall, M.C. Deans, Recommended figures of merit for green monopropellants, in: 49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, 2013, p. 3722.
3. V. Bombelli, D. Simon, J.-L. Moerel, T. Marée, Economic benefits of the use of non-toxic mono-propellants for spacecraft applications, in: 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2003, p. 4783.
4. New technologies for ammonium dinitramide based monopropellant thrusters–The project RHEFORM;Negri;Acta Astronaut.,2018
5. Formulation and characterization of ADN-based liquid monopropellants;Wingborg,2004