Analysis and observation of spacecraft plume/ionosphere interactions during maneuvers of the space shuttle
dc.contributor.author | Stephani, K. A. | en_US |
dc.contributor.author | Boyd, I. D. | en_US |
dc.contributor.author | Balthazor, R. L. | en_US |
dc.contributor.author | McHarg, M. G. | en_US |
dc.contributor.author | Mueller, B. A. | en_US |
dc.contributor.author | Adams, R. J. | en_US |
dc.date.accessioned | 2014-11-04T16:35:32Z | |
dc.date.available | WITHHELD_11_MONTHS | en_US |
dc.date.available | 2014-11-04T16:35:32Z | |
dc.date.issued | 2014-09 | en_US |
dc.identifier.citation | Stephani, K. A.; Boyd, I. D.; Balthazor, R. L.; McHarg, M. G.; Mueller, B. A.; Adams, R. J. (2014). "Analysis and observation of spacecraft plume/ionosphere interactions during maneuvers of the space shuttle." Journal of Geophysical Research: Space Physics 119(9): 7636-7648. | en_US |
dc.identifier.issn | 2169-9380 | en_US |
dc.identifier.issn | 2169-9402 | en_US |
dc.identifier.uri | https://hdl.handle.net/2027.42/109306 | |
dc.description.abstract | This work employs in situ measurement data and constructive simulations to examine the underlying physical mechanisms that drive spacecraft plume interactions with the space environment in low‐Earth orbit. The study centers on observations of the enhanced flux of plasma generated during a maneuver of Space Shuttle Endeavour as part of the Sensor Test for Orion Relative Navigation Risk Mitigation experiment in May 2011. The Canary electrostatic analyzer (ESA) instrument mounted on the portside truss of the International Space Station indicated an elevated ion current during the shuttle maneuver. The apparent source of enhanced ion current is a result of interaction of the spacecraft thruster plume with the rarefied ambient ionosphere, which generates regions of relatively high density plasma through charge exchange between the neutral plume and ambient ions. To reconstruct this event, unsteady simulation data were generated using a combined direct simulation Monte Carlo/particle‐in‐cell methodology, which employed detailed charge exchange cross‐section data and a magnetic field model. The simulation provides local plasma characteristics at the ESA sensor location, and a sensor model is subsequently used to transform the local properties into a prediction of measured ion current. The predicted and observed total currents are presented as a function of time over a 30 s period of pulsed thruster firings. A strong correlation is observed in the temporal characteristics of the simulated and measured total current, and good agreement is also achieved in the total current predicted by the model. These results support conclusions that (1) the enhanced flux of plasma observed by the ESA instrument is associated with Space Shuttle thruster firings and (2) the simulation model captures the essential features of the plume interactions based on the observation data. Key Points Plumes interact with LEO plasma/B‐field Thruster burns associated with enhanced plasma flux Simulation model reproduces in situ observation data | en_US |
dc.publisher | Wiley Periodicals, Inc. | en_US |
dc.publisher | Oxford Univ. Press | en_US |
dc.subject.other | Spacecraft Plume Interaction | en_US |
dc.subject.other | Direct Simulation Monte Carlo | en_US |
dc.subject.other | Particle‐In‐Cell | en_US |
dc.subject.other | Unsteady Plumes | en_US |
dc.subject.other | Ionosphere | en_US |
dc.subject.other | Electrostatic Analyzer | en_US |
dc.title | Analysis and observation of spacecraft plume/ionosphere interactions during maneuvers of the space shuttle | en_US |
dc.type | Article | en_US |
dc.rights.robots | IndexNoFollow | en_US |
dc.subject.hlbsecondlevel | Astronomy and Astrophysics | en_US |
dc.subject.hlbtoplevel | Science | en_US |
dc.description.peerreviewed | Peer Reviewed | en_US |
dc.description.bitstreamurl | http://deepblue.lib.umich.edu/bitstream/2027.42/109306/1/jgra51246.pdf | |
dc.identifier.doi | 10.1002/2013JA019476 | en_US |
dc.identifier.source | Journal of Geophysical Research: Space Physics | en_US |
dc.identifier.citedreference | Birdsall, C., and A. Langdon ( 2004 ), Plasma Physics via Computer Simulation, Taylor and Francis, New York. | en_US |
dc.identifier.citedreference | Burke, W., L. Gentile, J. Machuzak, D. Hardy, and D. Hunton ( 1995 ), Energy distributions of thruster pickup ions detected by the Shuttle Potential and Return Electron Experiments during TSS 1, J. Geophys. Res., 100 ( A10 ), 19,773 – 19,790, doi: 10.1029/95JA01214. | en_US |
dc.identifier.citedreference | Dressler, R., M. Bastian, D. Levandier, and E. Murad ( 1996 ), Empirical model of the state‐to‐state dynamics in near‐resonant hyperthermal X+ + H2O charge‐transfer reactions, Int. J. Mass Spectrom. Ion Processes, 159, 245 – 256. | en_US |
dc.identifier.citedreference | Drakes, J., and D. Swann ( 1999 ), DSMC computations of the Progress‐M spacecraft retrofiring exhaust plume, paper presented at AIAA Aerospace Sciences Meeting (37th) and Exhibit, Paper No. AIAA – 99‐0975, Ft. Belvoir Defense Technical Information Center, Reno, Nev. on January 11‐14, 1999. | en_US |
dc.identifier.citedreference | Dahl, D., and J. Delmore ( 1987 ), The SIMION PCI/PS2 User's Manual Version 3.1, Idaho National Engineering Laboratory, Idaho Falls. | en_US |
dc.identifier.citedreference | Cai, C. ( 2005 ), Theoretical and numerical studies of plume flows in vacuum chambers, PhD dissertation, Univ. of Michigan, Ann Arbor, Mich. | en_US |
dc.identifier.citedreference | Bernhardt, P., et al. ( 2012 ), Ground and space‐based measurement of rocket engine burns in the ionosphere, IEEE Trans. Plasma Sci., 40 ( 5 ), 1267 – 1286. | en_US |
dc.identifier.citedreference | Bird, G. ( 1994 ), Molecular Gas Dynamics and the Direct Simulation of Gas Flows, Oxford Univ. Press, Oxford, U. K. | en_US |
dc.identifier.citedreference | Boyd, I., and R. Dressler ( 2002 ), Far field modeling of the plasma plume of a Hall thruster, J. Appl. Phys., 92 ( 4 ), 1764 – 1774. | en_US |
dc.identifier.citedreference | Stuit, T. ( 2011 ), Designing the STS‐134 re‐rendezvous: A preparation for future crewed rendezvous missions, paper presented at AIAA SPACE 2011 Conference Exposition Online Proceedings, AIAA Paper No. 2011‐7189, Timothy Stuit United Space Alliance, Houston, Tex. | en_US |
dc.identifier.citedreference | Stephani, K., and I. Boyd ( 2014 ), Detailed modeling and analysis of spacecraft plume/ionosphere interactions in low Earth orbit, J. Geophys. Res. Space Physics, 119, 2101 – 2116, doi: 10.1002/2013JA019222. | en_US |
dc.identifier.citedreference | McMahon, W., R. Salter, R. Hills, and D. Delorey ( 1983 ), Measured electron contribution to shuttle plasma environment, paper presented at Shuttle Environment and Operations Meeting, AIAA Paper No. AIAA‐83‐2598, Washington, D. C. | en_US |
dc.identifier.citedreference | Lindsay, B., R. Rejoub, D. Sieglaff, and R. Stebbings ( 2001 ), Charge transfer of keV O + ions with CO and H 2 O, J. Phys. B: At., Mol. Opt. Phys., 34, 2159, doi: 10.1088/0953‐4075/34/11/308. | en_US |
dc.identifier.citedreference | Li, X., Y.‐L. Huang, G. Flesch, and C. Ng ( 1995 ), Absolute total cross sections for the ion‐molecule reaction O + ( 4 S o )+H 2 O, J. Chem. Phys., 102 ( 5100–5101 ). | en_US |
dc.identifier.citedreference | Kelley, M. C. ( 1989 ), The Earth's Ionosphere, Acad. Press, San Diego, Calif. | en_US |
dc.identifier.citedreference | Karabadzhak, G., Y. Plastinin, B. Khmelinin, V. Teslenko, N. Shvets, J. Drakes, D. Swann, and W. McGregor ( 1997 ), Experimentation using the Mir station as a space laboratory, paper presented at AIAA Aerospace Sciences Meeting, Reno, Nev., AIAA Paper No. AIAA‐97‐0288. | en_US |
dc.identifier.citedreference | Kaplan, C., and P. Bernhardt ( 2010 ), Effect of an altitude‐dependent background atmosphere on shuttle plumes, J. Spacecr. Rockets, 47 ( 4 ), 700 – 704. | en_US |
dc.identifier.citedreference | Feldmesser, H., M. Darrin, R. Osiander, L. Paxton, A. Rogers, J. Marks, M. McHarg, R. Balthazor, L. Krause, and J. FitzGerald ( 2010 ), Canary: Ion spectroscopy for ionospheric sensing, paper presented at SPIE 7691, Space Missions and Technologies, Orlando, Fla., doi: 10.1117/12.850414. | en_US |
dc.identifier.citedreference | Turner, B., and J. Rutherford ( 1968 ), Charge transfer and ion‐atom interchange reactions of water vapor ions, J. Geophys. Res., 73, 6751 – 6758. | en_US |
dc.identifier.citedreference | Enloe, C., K. Habush, R. Haaland, T. Patterson, C. Richardson, C. Lazidis, and R. Whiting ( 2003 ), Miniaturized electrostatic analyzer manufactured using photolithographic etching, Rev. Sci. Instrum., 74 ( 3 ), 1192 – 1195. | en_US |
dc.owningcollname | Interdisciplinary and Peer-Reviewed |
Files in this item
Remediation of Harmful Language
The University of Michigan Library aims to describe library materials in a way that respects the people and communities who create, use, and are represented in our collections. Report harmful or offensive language in catalog records, finding aids, or elsewhere in our collections anonymously through our metadata feedback form. More information at Remediation of Harmful Language.
Accessibility
If you are unable to use this file in its current format, please select the Contact Us link and we can modify it to make it more accessible to you.