Evaluation of Afterburning Cessation Mechanisms in Fuel Rich Rocket Exhaust Plumes

doi 10.21236/ada404895
Full Text
Abstract

Available in full text

Date
Authors
Publisher

Defense Technical Information Center

Related search

The Suppression of Afterburning in Solid Rocket Plumes by Potassium Salts

1984English

Numerical Simulation of Ionized Rocket Plumes

Journal of Thermophysics and Heat Transfer
Condensed Matter PhysicsMechanical EngineeringSpaceFluid FlowPlanetary ScienceTransfer ProcessesAerospace Engineering
2014English

Numerical Simulation of Radiation in High Altitude Solid Propellant Rocket Plumes

Acta Astronautica
Aerospace Engineering
2019English

Effects of Rocket Exhaust Products in the Thermosphere and Ionsphere

1980English

Geomagnetic Effects Caused by Rocket Exhaust Jets

Solnecno-Zemnaa Fizika
Atmospheric SciencePlanetary ScienceGeophysicsSpace
2016English

Scale Model Tests of a Nuclear Rocket Exhaust Scrubber

1968English

Fuel Oxidation Efficiencies and Exhaust Composition in Solid Oxide Fuel Cells

English

Measurement of the Liquid Level in the Fuel Tank of Rocket

American Journal of Aerospace Engineering
2016English

Application of a Multiscale Particle Scheme to High Altitude Rocket Exhaust Flows

2009English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2026 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy