Solid fuel ramjet fuel optimization for maximum impulse-density with respect to air to fuel ratio and relative fuel regression rates derived from thermogravimetric analysis-Reference-Cited by-同舟云学术

Solid fuel ramjet fuel optimization for maximum impulse-density with respect to air to fuel ratio and relative fuel regression rates derived from thermogravimetric analysis

Published:2019-03 Issue: Volume:86 Page:478-486
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

McDonald Brian^ORCID,Rice Jeremy

Publisher

Elsevier BV

Subject

Aerospace Engineering

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4. Performance of an experimental polyethylene solid fuel ramjet;Gobbo-Ferreira;Acta Astronaut.,1999

5. Convective thermal ignition of an individual polymethylmethacrylate particle;Wang;J. Propuls. Power,1992

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