Voyager spacecraft. Volume VII - 1969 flight test spacecraft and OSE Study report, phase IA
Voyager spacecraft and operation support equipment design and program planning for flight test mission
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Voyager spacecraft and operation support equipment design and program planning for flight test mission
Voyager spacecraft preferred design
Preferred design for Voyager spacecraft subsystems
Voyager spacecraft implementation plan
Operational support equipment for Voyager spacecraft
Tradeoff analyses for Voyager spacecraft propulsion system selection
Mission objectives and systems design criteria for 1971 Voyager spacecraft concept
Functional descriptions of subsystems for 1971 Voyager flight spacecraft
Functional descriptions of Operational Support Equipment /OSE/ for preliminary design of Voyager spacecraft
Systems analysis study relating to applicability of several types of propulsion systems for Voyager missions
Earth-lunar horizon sensor program, design characteristics, and application of horizon sensors to Apollo extension system space missions
Response time and design requirements of earth- lunar horizon sensor program
Synthesis and characterization of vinylaromatic polymers
Elimination of rocket motor ignition by electrostatic initiation through development of electrically insensitive igniter and nonelectric stimulus transfer system
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Problems encountered in testing onboard signal processing hardware designed to achieve radiometric and geometric correction of satellite imaging data are considered. These include obtaining representative image and ancillary data for simulation and the transfer and storage of a large quantity of image data at very high speed. The high resolution, high speed preprocessing of LANDSAT-D imagery is considered.
It is pointed out that International Ultraviolet Explorer (IUE) data for several early A type supergiants are now available to complement the ground-based spectroscopic data available for these bright stars. An examination of the resonance doublet of Mg II in the A type supergiants reveals that HR 1040 (HD 21389) is the only star in the observational literature in which a violet-shifted, deep absorption line is present without complete saturation. From an unsaturated profile, a good estimate of Mg(+) density can be found by means of accurate radiative transfer calculations. A relation can then be derived between mass loss rate and ionization balance. When certain velocity-related quantities can be estimated from a Mg II line profile, the H-alpha provides an estimate of the mass loss rate. The present investigation is concerned with an application of these diagnostics to HR 1040.
It is argued that the bright supergiant star Mu Sagittarii is accompanied by a smaller and hotter star, of spectral type approximately B1.5 V. The single-line radial-velocity curve of the B8 star leads to a fairly large mass function, f(m) = 2.64 solar masses, implying that the companion should have at least 50 percent of the mass of the visible star. Older optical observations indicated the presence of a shallow eclipse at the time of the conjunction with the supergiant behind the companion. Since the Copernicus, IUE, and Voyager observations show that the companion is the hotter component, that eclipse must have been the secondary eclipse (if it was an eclipse at all). A deeper, primary eclipse has been predicted by Plavec in 1978. It was indeed observed as a marked decrease of the far-ultraviolet flux from the system both with the Copernicus and the IUE satellites. The presence of a hotter but smaller component in Mu Sagittarii offers a unique opportunity to study the outer atmospheric layers of a supergiant which is of a much earlier spectral type than the supergiants in the Zeta Aurigae systems.