EXTREME MODEL ATMOSPHERE OF MARS

Theoretical models of the atmosphere of Mars were computed on the basis of present factual knowledge with a minimum of assumptions. The resultant model atmosphere gives extreme upper and lower limits for pressure, temperature, and density in the Martian atmosphere up to 150 km altitude. While this r...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	Schilling, Gerhard F
Format:	Report
Sprache:	eng
Schlagworte:	Astronomy ATMOSPHERE MODELS ATMOSPHERES DENSITY ENGINEERING LIMITATIONS LOW LEVEL MARS PROBES MARS(PLANET) MATHEMATICAL ANALYSIS MATHEMATICAL MODELS PLANETARY ATMOSPHERES PRESSURE PROBES RELIABILITY SPACE PROBES TEMPERATURE
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

container_end_page
container_issue
container_start_page
container_title
container_volume
creator	Schilling, Gerhard F
description	Theoretical models of the atmosphere of Mars were computed on the basis of present factual knowledge with a minimum of assumptions. The resultant model atmosphere gives extreme upper and lower limits for pressure, temperature, and density in the Martian atmosphere up to 150 km altitude. While this rigorous method yielded reliable data needed for the engineering design of space probes, the spread of values is still extremely wide and indicative of the present scarcity of knowledge. Prepared for presentation at the 11th International Astrophysical Symposium, Liege, Belgium, 9-11 Jul 1962. Supported in part by the Jet Propulsion Lab., Calif. Inst. of Tech., Pasadena, Contract N33561 (NAS7 100) .
format	Report
fullrecord	<record><control><sourceid>dtic_1RU</sourceid><recordid>TN_cdi_dtic_stinet_AD0607504</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>AD0607504</sourcerecordid><originalsourceid>FETCH-dtic_stinet_AD06075043</originalsourceid><addsrcrecordid>eNrjZFBwjQgJcvV1VfD1d3H1UXAM8fUPDvBwDXJV8HdT8HUMCuZhYE1LzClO5YXS3Awybq4hzh66KSWZyfHFJZl5qSXxji4GZgbmpgYmxgSkAZ_gHtg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>EXTREME MODEL ATMOSPHERE OF MARS</title><source>DTIC Technical Reports</source><creator>Schilling, Gerhard F</creator><creatorcontrib>Schilling, Gerhard F ; RAND CORP SANTA MONICA CA</creatorcontrib><description>Theoretical models of the atmosphere of Mars were computed on the basis of present factual knowledge with a minimum of assumptions. The resultant model atmosphere gives extreme upper and lower limits for pressure, temperature, and density in the Martian atmosphere up to 150 km altitude. While this rigorous method yielded reliable data needed for the engineering design of space probes, the spread of values is still extremely wide and indicative of the present scarcity of knowledge. Prepared for presentation at the 11th International Astrophysical Symposium, Liege, Belgium, 9-11 Jul 1962. Supported in part by the Jet Propulsion Lab., Calif. Inst. of Tech., Pasadena, Contract N33561 (NAS7 100) .</description><language>eng</language><subject>Astronomy ; ATMOSPHERE MODELS ; ATMOSPHERES ; DENSITY ; ENGINEERING ; LIMITATIONS ; LOW LEVEL ; MARS PROBES ; MARS(PLANET) ; MATHEMATICAL ANALYSIS ; MATHEMATICAL MODELS ; PLANETARY ATMOSPHERES ; PRESSURE ; PROBES ; RELIABILITY ; SPACE PROBES ; TEMPERATURE</subject><creationdate>1962</creationdate><rights>Approved for public release; distribution is unlimited.</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,776,881,27546,27547</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/AD0607504$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Schilling, Gerhard F</creatorcontrib><creatorcontrib>RAND CORP SANTA MONICA CA</creatorcontrib><title>EXTREME MODEL ATMOSPHERE OF MARS</title><description>Theoretical models of the atmosphere of Mars were computed on the basis of present factual knowledge with a minimum of assumptions. The resultant model atmosphere gives extreme upper and lower limits for pressure, temperature, and density in the Martian atmosphere up to 150 km altitude. While this rigorous method yielded reliable data needed for the engineering design of space probes, the spread of values is still extremely wide and indicative of the present scarcity of knowledge. Prepared for presentation at the 11th International Astrophysical Symposium, Liege, Belgium, 9-11 Jul 1962. Supported in part by the Jet Propulsion Lab., Calif. Inst. of Tech., Pasadena, Contract N33561 (NAS7 100) .</description><subject>Astronomy</subject><subject>ATMOSPHERE MODELS</subject><subject>ATMOSPHERES</subject><subject>DENSITY</subject><subject>ENGINEERING</subject><subject>LIMITATIONS</subject><subject>LOW LEVEL</subject><subject>MARS PROBES</subject><subject>MARS(PLANET)</subject><subject>MATHEMATICAL ANALYSIS</subject><subject>MATHEMATICAL MODELS</subject><subject>PLANETARY ATMOSPHERES</subject><subject>PRESSURE</subject><subject>PROBES</subject><subject>RELIABILITY</subject><subject>SPACE PROBES</subject><subject>TEMPERATURE</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1962</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZFBwjQgJcvV1VfD1d3H1UXAM8fUPDvBwDXJV8HdT8HUMCuZhYE1LzClO5YXS3Awybq4hzh66KSWZyfHFJZl5qSXxji4GZgbmpgYmxgSkAZ_gHtg</recordid><startdate>196206</startdate><enddate>196206</enddate><creator>Schilling, Gerhard F</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>196206</creationdate><title>EXTREME MODEL ATMOSPHERE OF MARS</title><author>Schilling, Gerhard F</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_AD06075043</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1962</creationdate><topic>Astronomy</topic><topic>ATMOSPHERE MODELS</topic><topic>ATMOSPHERES</topic><topic>DENSITY</topic><topic>ENGINEERING</topic><topic>LIMITATIONS</topic><topic>LOW LEVEL</topic><topic>MARS PROBES</topic><topic>MARS(PLANET)</topic><topic>MATHEMATICAL ANALYSIS</topic><topic>MATHEMATICAL MODELS</topic><topic>PLANETARY ATMOSPHERES</topic><topic>PRESSURE</topic><topic>PROBES</topic><topic>RELIABILITY</topic><topic>SPACE PROBES</topic><topic>TEMPERATURE</topic><toplevel>online_resources</toplevel><creatorcontrib>Schilling, Gerhard F</creatorcontrib><creatorcontrib>RAND CORP SANTA MONICA CA</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Schilling, Gerhard F</au><aucorp>RAND CORP SANTA MONICA CA</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>EXTREME MODEL ATMOSPHERE OF MARS</btitle><date>1962-06</date><risdate>1962</risdate><abstract>Theoretical models of the atmosphere of Mars were computed on the basis of present factual knowledge with a minimum of assumptions. The resultant model atmosphere gives extreme upper and lower limits for pressure, temperature, and density in the Martian atmosphere up to 150 km altitude. While this rigorous method yielded reliable data needed for the engineering design of space probes, the spread of values is still extremely wide and indicative of the present scarcity of knowledge. Prepared for presentation at the 11th International Astrophysical Symposium, Liege, Belgium, 9-11 Jul 1962. Supported in part by the Jet Propulsion Lab., Calif. Inst. of Tech., Pasadena, Contract N33561 (NAS7 100) .</abstract><oa>free_for_read</oa></addata></record>
fulltext	fulltext_linktorsrc
identifier
ispartof
issn
language	eng
recordid	cdi_dtic_stinet_AD0607504
source	DTIC Technical Reports
subjects	Astronomy ATMOSPHERE MODELS ATMOSPHERES DENSITY ENGINEERING LIMITATIONS LOW LEVEL MARS PROBES MARS(PLANET) MATHEMATICAL ANALYSIS MATHEMATICAL MODELS PLANETARY ATMOSPHERES PRESSURE PROBES RELIABILITY SPACE PROBES TEMPERATURE
title	EXTREME MODEL ATMOSPHERE OF MARS
url	https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-23T07%3A20%3A39IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-dtic_1RU&rft_val_fmt=info:ofi/fmt:kev:mtx:book&rft.genre=unknown&rft.btitle=EXTREME%20MODEL%20ATMOSPHERE%20OF%20MARS&rft.au=Schilling,%20Gerhard%20F&rft.aucorp=RAND%20CORP%20SANTA%20MONICA%20CA&rft.date=1962-06&rft_id=info:doi/&rft_dat=%3Cdtic_1RU%3EAD0607504%3C/dtic_1RU%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true