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High specific impulse gas-core reactors
NTRS Full-Text: Click to View  [PDF Size: 1.2 MB]
Author and Affiliation:
Ragsdale, R. G.(NASA Lewis Research Center, Cleveland, OH, United States)
Abstract: Calculated estimates of gas core nuclear rocket engine weights for specific impulses ranging from 3000 to 7000 seconds and for engine thrusts ranging from 4400 to 440,000 newtons
Publication Date: Mar 01, 1971
Document ID:
19710010425
(Acquired Nov 22, 1995)
Accession Number: 71N19900
Subject Category: NUCLEAR ENGINEERING
Report/Patent Number: NASA-TM-X-2243, E-6087
Document Type: Technical Report
Publisher Information: WASHINGTON, United States
Contract/Grant/Task Num: 122-28
Financial Sponsor: NASA; United States
Organization Source: NASA Lewis Research Center; Cleveland, OH, United States
Description: 19p; In English
Distribution Limits: Unclassified; Publicly available; Unlimited
Rights: No Copyright
NASA Terms: GASEOUS FISSION REACTORS; NUCLEAR ROCKET ENGINES; ROCKET THRUST; SPECIFIC IMPULSE; PROPULSION SYSTEM PERFORMANCE; WEIGHT (MASS)
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