Polarimetry Studies of Ionospheric Modification by Rocket boosters
High altitude releases of certain molecules in booster rocket exhausts are known to deplete electron concentration in the ionosphere dramatically. These effects are exhibited in recent Faraday rotation measurement for the HEAO-C launch from Cape Kennedy on September 20, 1979 and the NOAA-B launch fr...
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creator | Reilly,M H Harnish,L O Goodman,John M |
description | High altitude releases of certain molecules in booster rocket exhausts are known to deplete electron concentration in the ionosphere dramatically. These effects are exhibited in recent Faraday rotation measurement for the HEAO-C launch from Cape Kennedy on September 20, 1979 and the NOAA-B launch from Vandenberg on May 29, 1980, in which total electron content drop-out responses to the booster rockets are evident. The polarimetry experiments and data for these nocturnal launches are presented, discussed, and analyzed to obtain time profiles of total electron content (TEC) associated with three different satellite-to-receiver raypaths. Calculations of the booster rocket effect are carried out in detail for the HEAO-C case in an attempt to theoretically simulate the experimental results for the early-time TEC depletion effect from the booster rocket. The calculational model includes a full, three-dimensional integration of the rocket exhaust effect, in which rocket exhaust expansion is treated as thermalized, mutual diffusion in the non-uniform ambient background atmosphere. Results are discussed, and future directions are indicated. (Author) |
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These effects are exhibited in recent Faraday rotation measurement for the HEAO-C launch from Cape Kennedy on September 20, 1979 and the NOAA-B launch from Vandenberg on May 29, 1980, in which total electron content drop-out responses to the booster rockets are evident. The polarimetry experiments and data for these nocturnal launches are presented, discussed, and analyzed to obtain time profiles of total electron content (TEC) associated with three different satellite-to-receiver raypaths. Calculations of the booster rocket effect are carried out in detail for the HEAO-C case in an attempt to theoretically simulate the experimental results for the early-time TEC depletion effect from the booster rocket. The calculational model includes a full, three-dimensional integration of the rocket exhaust effect, in which rocket exhaust expansion is treated as thermalized, mutual diffusion in the non-uniform ambient background atmosphere. Results are discussed, and future directions are indicated. (Author)</description><language>eng</language><subject>ATMOSPHERIC CHEMISTRY ; Atmospheric Physics ; BOOSTER ROCKET ENGINES ; Combustion and Ignition ; DEPLETION ; ELECTRON DENSITY ; EXHAUST GASES ; EXPANSION ; FARADAY EFFECT ; HIGH ALTITUDE ; IONOSPHERIC MODIFICATION ; MOLECULES ; PE61153N ; POLARIMETRY ; Rocket Engines ; ROTATION ; Test Facilities, Equipment and Methods ; WU0149</subject><creationdate>1981</creationdate><rights>APPROVED FOR PUBLIC RELEASE</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,780,885,27566,27567</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/ADA100371$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Reilly,M H</creatorcontrib><creatorcontrib>Harnish,L O</creatorcontrib><creatorcontrib>Goodman,John M</creatorcontrib><creatorcontrib>NAVAL RESEARCH LAB WASHINGTON DC</creatorcontrib><title>Polarimetry Studies of Ionospheric Modification by Rocket boosters</title><description>High altitude releases of certain molecules in booster rocket exhausts are known to deplete electron concentration in the ionosphere dramatically. These effects are exhibited in recent Faraday rotation measurement for the HEAO-C launch from Cape Kennedy on September 20, 1979 and the NOAA-B launch from Vandenberg on May 29, 1980, in which total electron content drop-out responses to the booster rockets are evident. The polarimetry experiments and data for these nocturnal launches are presented, discussed, and analyzed to obtain time profiles of total electron content (TEC) associated with three different satellite-to-receiver raypaths. Calculations of the booster rocket effect are carried out in detail for the HEAO-C case in an attempt to theoretically simulate the experimental results for the early-time TEC depletion effect from the booster rocket. The calculational model includes a full, three-dimensional integration of the rocket exhaust effect, in which rocket exhaust expansion is treated as thermalized, mutual diffusion in the non-uniform ambient background atmosphere. Results are discussed, and future directions are indicated. (Author)</description><subject>ATMOSPHERIC CHEMISTRY</subject><subject>Atmospheric Physics</subject><subject>BOOSTER ROCKET ENGINES</subject><subject>Combustion and Ignition</subject><subject>DEPLETION</subject><subject>ELECTRON DENSITY</subject><subject>EXHAUST GASES</subject><subject>EXPANSION</subject><subject>FARADAY EFFECT</subject><subject>HIGH ALTITUDE</subject><subject>IONOSPHERIC MODIFICATION</subject><subject>MOLECULES</subject><subject>PE61153N</subject><subject>POLARIMETRY</subject><subject>Rocket Engines</subject><subject>ROTATION</subject><subject>Test Facilities, Equipment and Methods</subject><subject>WU0149</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1981</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZHAKyM9JLMrMTS0pqlQILilNyUwtVshPU_DMz8svLshILcpMVvDNT8lMy0xOLMnMz1NIqlQIyk_OTi1RSMrPLy5JLSrmYWBNS8wpTuWF0twMMm6uIc4euiklmcnxxSWZeakl8Y4ujoYGBsbmhsYEpAF28C94</recordid><startdate>19810527</startdate><enddate>19810527</enddate><creator>Reilly,M H</creator><creator>Harnish,L O</creator><creator>Goodman,John M</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>19810527</creationdate><title>Polarimetry Studies of Ionospheric Modification by Rocket boosters</title><author>Reilly,M H ; Harnish,L O ; Goodman,John M</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADA1003713</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1981</creationdate><topic>ATMOSPHERIC CHEMISTRY</topic><topic>Atmospheric Physics</topic><topic>BOOSTER ROCKET ENGINES</topic><topic>Combustion and Ignition</topic><topic>DEPLETION</topic><topic>ELECTRON DENSITY</topic><topic>EXHAUST GASES</topic><topic>EXPANSION</topic><topic>FARADAY EFFECT</topic><topic>HIGH ALTITUDE</topic><topic>IONOSPHERIC MODIFICATION</topic><topic>MOLECULES</topic><topic>PE61153N</topic><topic>POLARIMETRY</topic><topic>Rocket Engines</topic><topic>ROTATION</topic><topic>Test Facilities, Equipment and Methods</topic><topic>WU0149</topic><toplevel>online_resources</toplevel><creatorcontrib>Reilly,M H</creatorcontrib><creatorcontrib>Harnish,L O</creatorcontrib><creatorcontrib>Goodman,John M</creatorcontrib><creatorcontrib>NAVAL RESEARCH LAB WASHINGTON DC</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Reilly,M H</au><au>Harnish,L O</au><au>Goodman,John M</au><aucorp>NAVAL RESEARCH LAB WASHINGTON DC</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Polarimetry Studies of Ionospheric Modification by Rocket boosters</btitle><date>1981-05-27</date><risdate>1981</risdate><abstract>High altitude releases of certain molecules in booster rocket exhausts are known to deplete electron concentration in the ionosphere dramatically. These effects are exhibited in recent Faraday rotation measurement for the HEAO-C launch from Cape Kennedy on September 20, 1979 and the NOAA-B launch from Vandenberg on May 29, 1980, in which total electron content drop-out responses to the booster rockets are evident. The polarimetry experiments and data for these nocturnal launches are presented, discussed, and analyzed to obtain time profiles of total electron content (TEC) associated with three different satellite-to-receiver raypaths. Calculations of the booster rocket effect are carried out in detail for the HEAO-C case in an attempt to theoretically simulate the experimental results for the early-time TEC depletion effect from the booster rocket. The calculational model includes a full, three-dimensional integration of the rocket exhaust effect, in which rocket exhaust expansion is treated as thermalized, mutual diffusion in the non-uniform ambient background atmosphere. Results are discussed, and future directions are indicated. (Author)</abstract><oa>free_for_read</oa></addata></record> |
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subjects | ATMOSPHERIC CHEMISTRY Atmospheric Physics BOOSTER ROCKET ENGINES Combustion and Ignition DEPLETION ELECTRON DENSITY EXHAUST GASES EXPANSION FARADAY EFFECT HIGH ALTITUDE IONOSPHERIC MODIFICATION MOLECULES PE61153N POLARIMETRY Rocket Engines ROTATION Test Facilities, Equipment and Methods WU0149 |
title | Polarimetry Studies of Ionospheric Modification by Rocket boosters |
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