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Radionuklid
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Radioisotope Generator for Use in the Voyager Spacecraft (Orbiter)
Baseline Configuration Selection, Voyager Task C
Rtg Parametric Study. Report for the Rtg Study, Voyager Task C
Preliminary Spacecraft Thermal Integration Analysis
Determination of Heat-Shield Char-Front Recession with a Nucleonic Technique
Uni-Directional Heat Rejection Rtg Parametric Study, Voyager Task C
Radioisojet Microthruster Test a Summary Report
Comparison Study of Rtg and Solar Powered Voyager Spacecraft, Voyager Task C
Rtg Spacecraft Mission Abort Study, Voyager Task C
Radiation Mapping of a Planetary Surface Lander System
Study of Separately Launched Multi-Use Space Electrical Power System. Midterm Technical Briefing
Advanced Electric Propulsion Research Semiannual Report, 31 Dec. 1967 - 30 Jun. 1968
Unmanned Spacecraft Rtg Shield Optimization Study Midterm Report
Pioneer F/G Program. Conduction of Exploratory Investigations Beyond the Orbit of Mars
Pioneer F/G Program. Conduction of Exploratory Investigations Beyond the Orbit of Mars
Power Systems for Spacecraft. Part I
Standardized Spacecraft: A Methodology for Decision Making. Ams Report No. 1199
Nuclear-Powered HYSAT Spacecraft: Comparative Design Study
Mission Environments for the Isotope Brayton Flight System (Preliminary)
Kilowatt Isotope Power System Phase II Plan. Volume II: Flight System Conceptual Design (FSCD)
Dynamic Isotope Power System (DIPS) Applications Study. Volume I. Summary. Final Report
General-Purpose Heat Source Development: Safety Verification Test Program. Flyer Plate Test Series
Aerial Systems Support for the Nevada Test Site Weapons Testing
Final Safety Analysis Report for the Galileo Mission: Volume 2. Summary
Final Safety Analysis Report for the Galileo Mission: Volume 1. Reference Design Document
Radiological risk analysis of potential SP-100 space mission scenarios
Final Safety Analysis Report 2 for the Galileo mission. Executive summary
Draft Environmental Impact Statement for the Galileo Mission (Tier 2)
Safety Testing Program for the Galileo Mission Radioisotope Thermoelectric Generator
General-Purpose Heat Source Development: Extended Series Test Program Large Fragment Tests
Development of the Power Sources for the Ulysses and Galileo Missions
NASA Low Power Dynamic Isotope Power System (DIPS) Conceptual Design Requirements Document
Draft Environmental Impact Statement for the Ulysses Mission (Tier 2)