Metal–organic frameworks as hypergolic additives for hybrid rockets-Reference-Cited by-同舟云学术

Metal–organic frameworks as hypergolic additives for hybrid rockets

Published:2022 Issue:12 Volume:13 Page:3424-3436
ISSN:2041-6520
Container-title:Chemical Science
language:en
Short-container-title:Chem. Sci.

Author:

Jobin Olivier¹^ORCID,Mottillo Cristina²,Titi Hatem M.³^ORCID,Marrett Joseph M.³,Arhangelskis Mihails⁴,Rogers Robin D.⁵,Elzein Bachar⁶,Friščić Tomislav³^ORCID,Robert Étienne¹^ORCID

Affiliation:

1. Department of Mechanical Engineering, Polytechnique Montréal, 2900 Boulevard Edouard-Montpetit, Montréal, QC H3T 1J4, Canada

2. ACSYNAM Inc., Montréal, QC H1P 1W1, Canada

3. Department of Chemistry, McGill University, 801 Sherbrooke Street West, Montréal, QC H2L 0B7, Canada

4. University of Warsaw, 1 Pasteura Street, Warsaw, 02-093, Poland

5. 525 Solutions, P.O. Box 2206, Tuscaloosa, Al 35403, USA

6. Reaction Dynamics, 45 Chemin de l’Aéroport, Saint-Jean-sur-Richelieu, QC J3B 7B5, Canada

Abstract

Hypergolic hybrid rocket propulsion, achieved through the addition of metal–organic frameworks, can contribute to reduce launch costs by simplifying engine design and operation.

Funder

Natural Sciences and Engineering Research Council of Canada

Canadian Space Agency

Publisher

Royal Society of Chemistry (RSC)

Subject

General Chemistry

Link

http://pubs.rsc.org/en/content/articlepdf/2022/SC/D1SC05975K

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5. Performance Analysis of a Low-Power Magnetically Shielded Hall Thruster: Experiments

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