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  • 1
    Publication Date: 2017-06-27
    Description: Solar proton forecast system and procedures used during Mariner 5 mission
    Keywords: SPACE RADIATION
    Type: NASA-CR-97807 , JPL-TR-32-1303
    Format: application/pdf
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  • 2
    Publication Date: 2016-06-07
    Description: Data on the electron environment trapped at Jupiter, tests performed to simulate the effects of electrons on Mariner, Jupiter-Saturn 1977 sensitive parts, and test results from those simulations, are summarized.
    Keywords: SPACE RADIATION
    Type: Dynatrend, Inc. Proc. of Outer Planet Probe Technol. Workshop, Sect. 1 through 11; 15 p
    Format: application/pdf
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  • 3
    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
    Format: text
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  • 4
    Publication Date: 2011-08-17
    Description: The simulation of radiation interference effects and the results of a radiation interference test on two Voyager Sun Sensor prototype detector assemblies are reported. The derivation of test levels and requirements are discussed and show that cobalt 60 gamma radiation is an effective and practical simulator of the ionization dose rate effects induced by high-energy electron flux incident on the spacecraft at a rate of 3.7 x 10 to the 8th e/sq cm-sec (10 rad(Si)/s) during closest approach to Jupiter. The test results provide information that is used to confirm an analytic correlation, and to predict satisfactory performance of a spacecraft sun sensing device having stringent angular resolution requirements. The measured detector response shows that at dose rates incident on the detector elements of 2 rad(Si)/sec, which is four times that expected during Jupiter encounter, the radiation-induced angle error is almost an order of magnitude less than that allowed by the acceptance criteria.
    Keywords: SPACECRAFT INSTRUMENTATION
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  • 5
    Publication Date: 2013-08-31
    Description: The effects of electron and proton radiation on spacecraft which will operate in the trapped radiation belts of the planet Jupiter are described, and the techniques and results of the testing and simulation used in the radiation effects program are discussed. Available data from the Pioneer 10 encounter of Jupiter are compared with pre-encounter models of the Jupiter radiation belts. The implications that the measured Jovian radiation belts have for future missions are considered.
    Keywords: ASTROPHYSICS
    Type: JPL-TM-33-708 , NASA-CR-140841
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  • 6
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    In:  Other Sources
    Publication Date: 2019-07-13
    Description: The paper describes the basis for current estimates of Shuttle environments. It considers available predictions of environments, uncertainties, worst-case conditions and discusses how this data base is used to derive the environmental design requirements. These requirements are assessed from a payload viewpoint, i.e., how they affect payload type, design, mission, location in Shuttle and payload classification. Finally, typical future Shuttle payloads (a pallet-mounted instrument and a spacecraft) are discussed relative to how the Shuttle environments influenced the payload design and test approach.
    Keywords: SPACE TRANSPORTATION
    Type: AIAA PAPER 81-0268 , Aerospace Sciences Meeting; Jan. 12-15, 1981; St. Louis, MO
    Format: text
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  • 7
    Publication Date: 2019-07-13
    Description: The effects of electron and proton radiation on spacecraft which will operate in the trapped radiation belts of the planet Jupiter are considered, and the techniques and results of the testing and simulation used in the radiation effects program at the Jet Propulsion Laboratory are discussed. Available data from the Pioneer 10 encounter of Jupiter are compared with pre-encounter models of the Jupiter radiation belts. The implications that the measured Jovian radiation belts have for future missions are considered.
    Keywords: LUNAR AND PLANETARY EXPLORATION
    Type: JPL-TM-33-708 , Evaluation of the effect of the space environment on materials; International Conference; June 17-21, 1974; Toulouse; France
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  • 8
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    Publication Date: 2019-07-13
    Description: A methodology for autonomous spacecraft design blends autonomy requirements with traditional mission requirements and assesses the impact of autonomy upon the total system resources available to support fault-tolerance and automation. A baseline functional design can be examined for autonomy implementation impacts, and the costs, risk, and benefits of various options can be assessed. The result of the process is a baseline design that includes autonomous control functions.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: IECEC ''84: Advanced energy systems - Their role in our future; August 19-24, 1984; San Francisco, CA
    Format: text
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