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Tuesday, May 5, 2020 | History

3 edition of Environmentally-induced discharge transient coupling to spacecraft found in the catalog.

Environmentally-induced discharge transient coupling to spacecraft

Viswanathan, R.

Environmentally-induced discharge transient coupling to spacecraft

by Viswanathan, R.

  • 195 Want to read
  • 25 Currently reading

Published by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, DC], [Springfield, Va .
Written in English

    Subjects:
  • Aerospace environments.,
  • Coupling circuits.,
  • Electric discharges.,
  • Electrical grounding.,
  • Plasma interaction experiment.,
  • Spacecraft charging.,
  • Surges.

  • Edition Notes

    Other titlesEnvironmentally induced discharge transient coupling to spacecraft.
    Statementby R. Viswanathan, G. Barbay, and N.J. Stevens.
    SeriesNASA contractor report -- NASA CR-174922.
    ContributionsBarbay, G., Stevens, N. J., United States. National Aeronautics and Space Administration.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL18083182M

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    slcet-tr (rev. ) ad-m This information can then be used to determine the response of the spacecraft electrical system to a surface discharge by means of lumped element models. The coupling into the electronics is assumed to be due to magnetic linkage from the transient currents flowing as a result of the discharge transient. The behavior of a spinning spacecraft.

    A further 1% is related to three accidental collisions, the Cosmos spacecraft with a Cosmos mission related object in December , the Cerise spacecraft with an Ariane H fragment in July , and a Thor stage with a CZ-4B stage fragment in January The Author: Gerald Griffith, Tateo Goka. 76 FR - Large Power Transformers From the Republic of Korea: Initiation of Antidumping Duty Investigation. Federal Register , , , ,


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Environmentally-induced discharge transient coupling to spacecraft by Viswanathan, R. Download PDF EPUB FB2

Get this from a library. Environmentally-induced discharge transient coupling to spacecraft. [R Viswanathan; G Barbay; N J Stevens; United States.

National Aeronautics and Space Administration.]. Eliminating coupling paths from a spark source to a victim will significantly lower the ESD threat. Coupling paths could be eliminated by separation, shielding, or filtering. Victim A victim is any part, component, subsystem, or elementof a spacecraft that can be adversely affected by an arc discharge (or field effects, in the case of someFile Size: 1MB.

More definitive data on environmentally induced Design Guidelines Format effects in geosynchronous satellites are needed, This data base could be obtained if all such spacecraft carried environment and event monitors (section ).

Spacecraft configuration Also of. A convoy of spacecraft is being considered, in which the lead spacecraft triggers detailed measurement of a very dynamic event by the following spacecraft.

Multiple concepts for distributed space telescopes and distributed synthetic apertures are proposed that rely heavily on coordination and control technologies developed under this subtopic.

The mechanism of space-plasma-induced discharge and its coupling with a large space power system are discussed. Data from both ground and flight experiments are reviewed to obtain an expected. A 'read' is counted each time someone views a publication summary (such as the title, abstract, and list of authors), clicks on a figure, or views or downloads the full-text.

Full text of "Project Apollo: A feasibility study of an advanced manned spacecraft and 9: Apollo program implementation plan" See other formats. 1 A.B. Carlson, Communication Systems, New York: McGraw Hill Book Company, 2 A.C Tribble, “The space environment, implications for spacecraft design”.

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The spacecraft solar array can degrade from 20% to 50% in power producing capability over a year mission depending upon the specific orbit it must operate in. These schemes have worked well for solar arrays, which are sized for end of spacecraft life conditions.

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As the temperature is changed, the thermal-transient effect distorts the static f vs. T characteristic, which leads to apparent hysteresis (see “Apparent Hysteresis” later in this chapter). The faster the temperature is changed, the larger is the contribution of the thermal-transient effect to the f vs.

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Coupling the hot deformation process directly to slabs at the continuous caster exit. A spark discharge between the tungsten electrodes was produced by a high-frequency Tesla coil with a voltage of 60, V.

The reaction time was usually a week or so and the maximum pressure bars. With this relatively simple experimental setup, Miller () was able to transform almost 50% of the original carbon (in the form of methane. Papers [] and a book [13] written between and were the first extensive works published on the science of spacecraft charging.

Phase Four This was dominated by the development of complex and sophisticated theories on spacecraft and plasma interactions. EFFECTIVE ACTIONS At very weak coupling, the best singleplaquette compact action is probably the one proposed by Manton, which for an SU(2) plaquette P is S = # 2 arccos 2 # 1 2 Tr(P) #.

(1) When the plaquette is close to the identity, this action is proportional to the square of the compact field strength and so resembles the classical action. Adam, Nico und Kampes, Bert und Eineder, Michael und Worawattanamateekul, Jirathana und Kircher, Michaela () The development of a scientific permanent scatterer system.

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