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  • 1
    Publication Date: 2011-08-16
    Description: Thermoelectric outer planet spacecraft /TOPS/ flight environment, systems design and Titan 3D/Centaur launch vehicle with Burner II upper stage
    Keywords: SPACE VEHICLES
    Type: ; ADEMIE DES SCIENCES
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  • 2
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    In:  Other Sources
    Publication Date: 2011-08-18
    Description: A Mariner Mark II spacecraft rendezvous mission with comet Kopff has been recommended by NASA's Solar System Exploration Committee, and is scheduled for a Shuttle launch in 1990. The spacecraft, which is scheduled to encounter the comet in 1994, will conduct a series of experiments including the study of the cometary nucleus, coma, and tail during perihelion passage; the determination of the nucleus and coma chemical/isotropic composition; the description of the nucleus's size, mass, rotation period, and pole occultation; distinctions of gas and dust hydrodynamics; and distinctions of solar wind interactions with the coma. The three-axis-stabilized spacecraft will be modular in design, and will incorporate a 490-Newton Insat engine, Viking Orbiter propulsion tanks, an Integrated Platform Pointing and Attitude Control Subsystem, and several scientific instruments. The spacecraft's Radio Frequency Subsystem will only use X-band telemetry with a downlink frequency of 8415 MHz, and an uplink frequency of 7161 MHz. The power sources in the present design include one radioisotope thermoelectric generator, three 3 Ah batteries, and a solar panel of approximately 7 sq m.
    Keywords: LAUNCH VEHICLES AND SPACE VEHICLES
    Type: (ISSN 0007-084X); 37; 361-365
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  • 3
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    In:  Other Sources
    Publication Date: 2011-08-19
    Description: Encompassing both an orbiter and an atmospheric probe, Project Galileo will study in detail the phenomena of the plant Jupiter together with those of its moons and its dynamic magnetospheric environment. The probe element will sample the temperature and pressure structure of the Jupiter atmosphere, analyzing the composition of its gases, locating the various cloud decks, measuring radiation balances, and searching for evidence of lightning strikes. Galileo is the first planetary exploration mission to be launched by means of the Space Shuttle. Virtually all Galileo subsystems are fully reprogrammable from the earth to allow mission alterations as new data are obtained. A major technical challenge, however, was posed by probe-to-orbiter communications through the dense Jovian atmosphere.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: IEEE Spectrum (ISSN 0018-9235); 22; 70-76
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  • 4
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    Publication Date: 2019-06-28
    Description: The Comet Rendezvous Asteroid Flyby (CRAF) spacecraft will be provided by the first Mariner Mark II (MMII). The MMII is a modular spacecraft which can be inexpensively reconfigured for different missions beyond the inner solar system. The rationale for a comet rendezvous mission are discussed, taking into account the probability that comets alone retain evidence of the chemical and physical conditions under which all solar system bodies were formed. A description of the rationale for the study of asteroids on the Comet Rendezvous Asteroid Flyby Mission is also presented. On its way to the rendezvous with a comet, the spacecraft will fly by one or more asteroids. It is assumed that the target asteroids will include moderately large main-belt objects several tens to perhaps 100 kilometers in diameter. Attention is also given to mission details, the spacecraft system, and the missions operations system.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: IAF PAPER 85-394
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  • 5
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    Publication Date: 2019-06-28
    Description: The concept used in the design of the Mariner Mark II (MMII) spacecraft is consistent with the solar system exploration strategies which were developed by the Space Science Board of the National Academy of Sciences. The missions to comets, main belt asteroids, and outer planets are sufficiently similar to make possible a use of almost all of the design, hardware, and software in most engineering subsystems, without significant modification, for subsequent missions. Mariner Mark II missions are discussed, taking into account a comet rendezvous with asteroid flyby, the Saturn Flyby/Titan Probe, the Cassini or Saturn Orbiter/Titan Probe, the Main Belt Asteroid Rendezvous mission, the Uranus Flyby/Uranus Probe mission, and the Neptune Flyby/Neptune Probe mission.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: AIAA PAPER 84-0214
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  • 6
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    Publication Date: 2019-07-27
    Description: The Mariner Jupiter/Saturn 1977 Spacecraft is designed to conduct a broad range of intensive investigations of the Jupiter and Saturn planetary systems, and of the interplanetary medium from earth to beyond Saturn. The spacecraft design has evolved from earlier Mariners, the Viking Orbiter, and the technology available for implementing long-life, reliable spacecraft designs. A description of the design is presented, and adaptations of that design for Jupiter/Uranus, Jupiter Orbiter, probe carrying, and mini-satellite carrying missions are discussed.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: AIAA PAPER 75-1155 , American Institute of Aeronautics and Astronautics and American Geophysical Union, Conference on the Exploration of the Outer Planets; Sept. 17-19, 1975; St. Louis, MO
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  • 7
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    Publication Date: 2019-07-13
    Description: Long life spacecraft design and reliability based on marine practices and advanced system technology project, considering grand tour outer planets mission
    Keywords: SPACE SCIENCES
    Type: AIAA PAPER 70-1247 , AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ANNUAL MEETING AND TECHNICAL DISPLAY, 7TH; Oct 19, 1970 - Oct 22, 1970; HOUSTON, TX
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