A model for the stability analysis of a gaseous core thermal nuclear rocket engine
type: CreativeWork
author: Steinkamp, Michael James
language: eng
keywords: Mechanical engineering, Astronomy, Turbulent mixing, Nuclear rocket engine, Fast and thermal reflector flux, Critical wave length
date published: 1995
date modified: 2026-07-22T22:25:00Z
provider: University of Illinois - Urbana-Champaign
publisher: Networked Digital Library of Theses and Dissertations
type: WebPage
source organization: University of Illinois at Urbana-Champaign

PropertyValue
property ID: Handle
value: https://hdl.handle.net/2142/123349