3 edition of Environmentally-induced discharge transient coupling to spacecraft found in the catalog.
Environmentally-induced discharge transient coupling to spacecraft
by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, DC], [Springfield, Va
Written in English
|Other titles||Environmentally induced discharge transient coupling to spacecraft.|
|Statement||by R. Viswanathan, G. Barbay, and N.J. Stevens.|
|Series||NASA contractor report -- NASA CR-174922.|
|Contributions||Barbay, G., Stevens, N. J., United States. National Aeronautics and Space Administration.|
|The Physical Object|
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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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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”.
3 Adv. Mater., Ring-opening polymerization of a silaferrocenophane within the channels of mesoporous silica: Poly (ferrocenylsilane)-mcm presursors to magnetic iron manostruc- tures,” Adv. Mater., vol. 10, pp.PDF; PDF; Print; Help NASA SBIR/STTR Program Support For questions about the NASA SBIR/STTR solicitations, the proposal preparation and electronic submission process, and other program related areas, please contact the NASA SBIR/STTR Program Support Office.
Phone: Email: [email protected] NASA SBIR/STTR Program Support is available Monday through Friday from. Full text of "NASA Technical Reports Server (NTRS) Fifth Annual Workshop on Space Operations Applications and Research (SOAR ), volume 2" See other formats.
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.
Proc. SPIESmart Structures and Materials Smart Structures and Integrated Systems, pg 1 (26 July ); doi: / Predicting the Reliability of Ceramics Under Transient Loads and Temperatures with CARES/Life: High Cycle Variable Amplitude Fatigue of a Nodular Cast Iron: On the Causes of Deviation from the Palmgren-Miner Rule: Prediction of Crack Growth Under Variable-Amplitude and Spectrum Loading in.
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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.
T performance. International Journal of Engineering and Applied Sciences is an international premier peer reviewed open access engineering and technology journal promoting the discovery, innovation, advancement and dissemination of basic and transitional knowledge in engineering, technology and related disciplines.
Materials of Engineering BY ‘‘Handbook of Chemistry and Physics,’’ Chemical Rubber Co. ‘‘Book of ASTM Standards,’’ ASTM. ‘‘ASHRAE Refrigeration Data Book,’’ ASHRAE. but if practices permit, they may be charged hot to save energy.
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  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.
In: Proceedings of the Joint ISPRS/EARSeL Workshop “High Resolution Mapping from Space ”. ISPRS. ISPRS Workshop High Resolution Mapping from Space, OctHannover, Germany.A rectangular room remains the ped'ect tex t - A more use ful represe ntation specifies the asy mptotic book teaching exampl e.
iven frequency f, eigentone density N, per hem at a g Intractable Simulations which is given by Given the painful consequ ences of constructing a real dN F rt hall with serious acousti ca l design defects, as.Toggle navigation.
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