Low-power, low level analog-to-digital converter for space vehicle applications
Low power, low level analog-to-digital converter for space vehicle applications
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Low power, low level analog-to-digital converter for space vehicle applications
Guidelines on space and planetary environment criteria for use in space vehicle development are provided. Information is incorporated in the disciplinary areas of atmospheric and ionospheric properties, radiation, geomagnetic field, astrodynamic constants, and meteoroids for the Earth's atmosphere above 90 km, interplanetary space, and the atmosphere and surfaces (when available) of the Moon and the planets (other than Earth) of this solar system. The Sun, Terrestrial Space, the Moon, Mercury, Venus, and Mars are covered.
The purpose of this report is twofold: (1) to survey the established analytic procedures for the simulation of controlled flexible space vehicles, and (2) to develop in detail methods that employ a combination of discrete and distributed ("modal") coordinates, i.e., the hybrid-coordinate methods. Analytic procedures are described in three categories: (1) discrete-coordinate methods, (2) hybrid-coordinate methods, and (3) vehicle normal-coordinate methods. Each of these approaches is described and analyzed for its advantages and disadvantages, and each is found to have an area of applicability. The hybrid-coordinate method combines the efficiency of the vehicle normal-coordinate method with the versatility of the discrete-coordinate method, and appears to have the widest range of practical application. The results in this report have practical utility in two areas: (1) complex digital computer simulation of flexible space vehicles of arbitrary configuration subject to realistic control laws, and (2) preliminary control system design based on transfer functions for linearized models of dynamics and control laws.
Role of liquid sloshing in attitude stability equations of liquid propellant space vehicles
Errors from geometric approximations of three computational models for space vehicle electron dose prediction
Man-machine interaction during prelaunch testing and checkout of space vehicles
Computer programs for shielding problems in manned space vehicles - proton penetration codes
Cosmic ray shower production in manned space vehicles - copper
Tracking, communications, and orbit determination for lunar space vehicles
NASA program for microelectronic circuit and space vehicle reliability
Lift penetration and growth effects on space vehicle response based on slender body theory
Mathematical models for determining microwave breakdown in space vehicles
Operational experience of Saturn/Apollo space vehicle checkout and launch
Automatic checkout systems for Saturn 5 manned space vehicle stages
Electromagnetic compatibility verification for Centaur and Surveyor space vehicles
Inflatable solar shields for thermal protection of space vehicles utilizing cryogen propellants
Space vehicle response to in-flight wind turbulence, describing operational procedure for launch advisability determination
Development and characteristics of self supporting space vehicle