A Model for the Stability Analysis of a Gaseous Core Thermal Nuclear Rocket Engine
type: CreativeWork
description: Made available in DSpace on 2017-07-06T18:58:56Z (GMT). No. of bitstreams: 3 Steinkamp_Michael_J_MS.pdf: 41676962 bytes, checksum: 43eca9280b78149c2adf55bbbdafe203 (MD5) Steinkamp_Michael_J_MS_ABS.pdf: 742907 bytes, checksum: f80614937c31a79d4c727932044b83d3 (MD5) license.txt: 4813 bytes, checksum: 715c4321821a960fa1a1e91d2ac7ebce (MD5) Previous issue date: 1992
abstract: Made available in DSpace on 2017-07-06T18:58:56Z (GMT). No. of bitstreams: 3 Steinkamp_Michael_J_MS.pdf: 41676962 bytes, checksum: 43eca9280b78149c2adf55bbbdafe203 (MD5) Steinkamp_Michael_J_MS_ABS.pdf: 742907 bytes, checksum: f80614937c31a79d4c727932044b83d3 (MD5) license.txt: 4813 bytes, checksum: 715c4321821a960fa1a1e91d2ac7ebce (MD5) Previous issue date: 1992
author: Steinkamp, Michael J.
language: en
keywords: nuclear engineering, rocket engine, thermal nuclear, stability analysis, gas core
date published: 2017-07-06T18:58:56Z
date modified: 2026-07-22T22:26:38Z
provider: University of Illinois - Urbana-Champaign
publisher: Networked Digital Library of Theses and Dissertations
type: WebPage
source organization: University of Illinois - Urbana-Champaign

PropertyValue
property ID: Handle
value: http://hdl.handle.net/2142/96549