Nuclear shuttle system definition study. Volume 6 - Reliability and safety analysis, phase 3 Final report, 1 May 1970 - 1 May 1971
Reliability and safety analysis of reusable nuclear stage space shuttle system
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Reliability and safety analysis of reusable nuclear stage space shuttle system
Working data from functional analysis and operations analysis of reusable nuclear stage space shuttle system
Description of design reference model for space shuttle propulsion system onboard checkout and monitoring equipment to establish design criteria - Vol. 2
Design, development, and characteristics of photoheliograph for use with Apollo telescope mount mission
New element preprocessor for NASTRAN programming to generate tables and routines for new elements
Data bus for avionics system of space shuttle, noting functions of interface unit, error detection and recovery, redundancy, and bus control philosophy
Evaluation of oxygen-hydrogen auxiliary propulsion subsystems for space shuttle booster and orbiter baseline vehicles
Pumped liquid, dual gas generation cycle for space shuttle booster and orbiter auxiliary propulsion systems
Common module series for NASA candidate experiment program for manned space stations in 1975-1985 era, discussing configuration and subsystem design
Space station thermal control system design, verifying radiator adequacy by parametric computer analysis with allowance for thermal coating degradation, vehicle attitude and other variables
A program was defined which consists of extended ground-based manned tests of regenerative life support systems. The tests are to evaluate prototypes of advanced life support systems under operational, integrated conditions, thus providing data for the design of efficient environmental control and life support systems for use in long-duration space missions. The requirements are defined for test operations to provide a simulation of an orbiting space laboratory. The features of Phase A and B programs are described. These tests use proven backup equipment to ensure successful evaluation of the advanced subsystems. A pre-tests all-systems checkout period is provided to minimize equipment problems during extended testing and to familiarize all crew and operating staff members with test equipment and procedures.
A preliminary plan and procedure are presented for conducting an extended manned test program for a regenerative life support system. Emphasis will be placed on elements associated with long-term system operation and long-term uninterrupted crew confinement.
Lunar soil simulation and stabilization, and impact penetrometer studies
The soil deformation mode under the action of a rolling sphere (boulder) was determined, and a theory based on actual soil failure mechanism was developed which provides a remote reconnaissance technique for study of soil conditions using boulder track observations. The failure mechanism was investigated by using models and by testing an instrumented spherical wheel. The wheel was specifically designed to measure contact pressure, but it also provided information on the failure mechanism. Further tests included rolling some 200 spheres down sand slopes. Films were taken of the rolling spheres, and the tracks were measured. Implications of the results and reevaluation of the lunar boulder tracks are discussed.
Borehole jacks for studying lunar soils and rocks
Permeability probe for measuring fluid flow through porous lunar surface materials
Research on the mechanics of lunar soils and on developing probes to determine the properties of lunar surface materials is summarized. The areas of investigation include the following: soil simulation, soil property determination using an impact penetrometer, soil stabilization using urethane foam or phenolic resin, effects of rolling boulders down lunar slopes, design of borehole jack and its use in determining failure mechanisms and properties of rocks, and development of a permeability probe for measuring fluid flow through porous lunar surface materials.
The objective of the relativity satellite mission is to perform an experiment in which a gyroscope in motion about the earth undergoes precession, presumably relativistic, with respect to the fixed stars. Performance of this experiment would clearly test the general theory of relativity and its various modifications. This is the only experiment suggested to date which would confirm the existence of motional drift as well. A mission is defined in which the measurement of the geodetic effect term to 0.2 arc sec/yr is achievable and the measurement of both geodetic and motional drift terms to an accuracy of 0.001 arc sec/yr may be possible. The design of the flying dewar satellite needed to maintain the experiment at cryogenic temperatures is discussed. The gyroscopes, magnetometer, and optical contacting method for dimensional stability of the experimental assembly are considered.