Room-temperature catalytically reactive ammonium dinitramide–H2O2 monopropellant for microsatellites-Reference-Cited by-同舟云学术

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Room-temperature catalytically reactive ammonium dinitramide–H2O2 monopropellant for microsatellites

Published:2022-02 Issue:3 Volume:69 Page:1631-1644
ISSN:0273-1177
Container-title:Advances in Space Research
language:en
Short-container-title:Advances in Space Research

Author:

Kim Ju Won,Bhosale Vikas Khandu,Kim Kyu-Seop,Lee Seungho,Kwon Sejin

Funder

Kementerian Pendidikan Malaysia

National Research Foundation of Korea

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference56 articles.

1. Flight demonstration of new thruster and green propellant technology on the PRISMA satellite;Anflo;Acta Astronaut.,2009

2. Anflo, K., Wingborg, N., 2000. Dinitramide based liquid mono-propellants. Patent WO0050363.

3. Review of formation flying and constellation missions using nanosatellites;Bandyopadhyay;J. Spacecraft Rockets,2016

4. Very-small-satellite design for distributed space missions;Barnhart;J. Spacecraft Rockets,2007

5. Ionic liquid and biofuel blend: a low–cost and high performance hypergolic fuel for propulsion application;Bhosale;ChemistrySelect,2016

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1. Lab-on-PCB technology for liquid monopropellant microthrusters: Design, fabrication, and performance evaluation;Sensors and Actuators A: Physical;2024-07

2. Electrical ignition of ADN-based green liquid propellant in constant volume combustion chamber and continuous flow;Advances in Space Research;2024-07

3. Technical Development in Ionic Liquid Monopropellant Ignition Using Plasma;Journal of the Korean Society of Propulsion Engineers;2024-06-30

4. Conceptual demonstration of a Lego-like modular fabrication method for an engineering model of a small monopropellant PCB thrusters;Acta Astronautica;2024-06

5. Effects of ignition voltage and electrode structure on electric ignition and combustion characteristics of Ammonium Dinitramide (ADN)-based liquid propellants in electric ignition mode in inert gas environment;Chinese Journal of Aeronautics;2024-04

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