DESIGN, DEVELOPMENT AND FLIGHT TEST OF THE VIPER DART ROBIN METEOROLOGICAL ROCKET SYSTEM
The Viper Dart Robin Meteorological Rocket System has been developed to obtain high altitude density and wind data by utilizing the Robin inflatable sphere as a sensing device. The system consists of a rocket motor, an unpowered dart, and the Robin inflatable sphere. Flight tests of the system provi...
Gespeichert in:
Hauptverfasser: | , |
---|---|
Format: | Report |
Sprache: | eng |
Schlagworte: | |
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 | Bollermann,Bruce Walker,Robert L |
description | The Viper Dart Robin Meteorological Rocket System has been developed to obtain high altitude density and wind data by utilizing the Robin inflatable sphere as a sensing device. The system consists of a rocket motor, an unpowered dart, and the Robin inflatable sphere. Flight tests of the system provided density, temperature, pressure and wind data from an altitude of about 90 kilometers to an altitude of approximately 40 kilometers or less. (Author) |
format | Report |
fullrecord | <record><control><sourceid>dtic_1RU</sourceid><recordid>TN_cdi_dtic_stinet_AD0675608</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>AD0675608</sourcerecordid><originalsourceid>FETCH-dtic_stinet_AD06756083</originalsourceid><addsrcrecordid>eNqFyb0KwjAUQOEsDqK-gcN9AIWCWF1jc_ODSW5JLkWnIlqhIC7N-6ODu9OB78zFRWF2Jm5AYYee2oCRQUYF2jtjGRgzA2lgi9C5FhMomRgSnVyEgIyUyJNxjfRfbM7IkK-ZMSzF7Hl7TcPq14VYa-TGbh9lvPdTGd9D6aWq6sO-ro67P_sD7QouNw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>DESIGN, DEVELOPMENT AND FLIGHT TEST OF THE VIPER DART ROBIN METEOROLOGICAL ROCKET SYSTEM</title><source>DTIC Technical Reports</source><creator>Bollermann,Bruce ; Walker,Robert L</creator><creatorcontrib>Bollermann,Bruce ; Walker,Robert L ; SPACE DATA CORP PHOENIX ARIZ</creatorcontrib><description>The Viper Dart Robin Meteorological Rocket System has been developed to obtain high altitude density and wind data by utilizing the Robin inflatable sphere as a sensing device. The system consists of a rocket motor, an unpowered dart, and the Robin inflatable sphere. Flight tests of the system provided density, temperature, pressure and wind data from an altitude of about 90 kilometers to an altitude of approximately 40 kilometers or less. (Author)</description><language>eng</language><subject>ACQUISITION RADAR ; AERODYNAMIC HEATING ; APOGEE ; DESCENT TRAJECTORIES ; FLIGHT TESTING ; FLUID DYNAMICS ; GROUND SUPPORT EQUIPMENT ; GUIDED MISSILE LAUNCHERS ; GUIDED MISSILE RANGES ; IMPACT PREDICTION ; METEOROLOGICAL BALLOONS ; METEOROLOGICAL PHENOMENA ; Meteorology ; PERFORMANCE(ENGINEERING) ; RADAR BEACONS ; RADAR CONFUSION REFLECTORS ; RADAR TRACKING ; Rockets ; SOLID PROPELLANT ROCKET ENGINES ; SOUNDING ROCKETS ; TELEMETER SYSTEMS ; UPPER ATMOSPHERE ; VIPER ROCKETS</subject><creationdate>1968</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>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,778,883,27554,27555</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/AD0675608$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Bollermann,Bruce</creatorcontrib><creatorcontrib>Walker,Robert L</creatorcontrib><creatorcontrib>SPACE DATA CORP PHOENIX ARIZ</creatorcontrib><title>DESIGN, DEVELOPMENT AND FLIGHT TEST OF THE VIPER DART ROBIN METEOROLOGICAL ROCKET SYSTEM</title><description>The Viper Dart Robin Meteorological Rocket System has been developed to obtain high altitude density and wind data by utilizing the Robin inflatable sphere as a sensing device. The system consists of a rocket motor, an unpowered dart, and the Robin inflatable sphere. Flight tests of the system provided density, temperature, pressure and wind data from an altitude of about 90 kilometers to an altitude of approximately 40 kilometers or less. (Author)</description><subject>ACQUISITION RADAR</subject><subject>AERODYNAMIC HEATING</subject><subject>APOGEE</subject><subject>DESCENT TRAJECTORIES</subject><subject>FLIGHT TESTING</subject><subject>FLUID DYNAMICS</subject><subject>GROUND SUPPORT EQUIPMENT</subject><subject>GUIDED MISSILE LAUNCHERS</subject><subject>GUIDED MISSILE RANGES</subject><subject>IMPACT PREDICTION</subject><subject>METEOROLOGICAL BALLOONS</subject><subject>METEOROLOGICAL PHENOMENA</subject><subject>Meteorology</subject><subject>PERFORMANCE(ENGINEERING)</subject><subject>RADAR BEACONS</subject><subject>RADAR CONFUSION REFLECTORS</subject><subject>RADAR TRACKING</subject><subject>Rockets</subject><subject>SOLID PROPELLANT ROCKET ENGINES</subject><subject>SOUNDING ROCKETS</subject><subject>TELEMETER SYSTEMS</subject><subject>UPPER ATMOSPHERE</subject><subject>VIPER ROCKETS</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1968</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNqFyb0KwjAUQOEsDqK-gcN9AIWCWF1jc_ODSW5JLkWnIlqhIC7N-6ODu9OB78zFRWF2Jm5AYYee2oCRQUYF2jtjGRgzA2lgi9C5FhMomRgSnVyEgIyUyJNxjfRfbM7IkK-ZMSzF7Hl7TcPq14VYa-TGbh9lvPdTGd9D6aWq6sO-ro67P_sD7QouNw</recordid><startdate>19680630</startdate><enddate>19680630</enddate><creator>Bollermann,Bruce</creator><creator>Walker,Robert L</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>19680630</creationdate><title>DESIGN, DEVELOPMENT AND FLIGHT TEST OF THE VIPER DART ROBIN METEOROLOGICAL ROCKET SYSTEM</title><author>Bollermann,Bruce ; Walker,Robert L</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_AD06756083</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1968</creationdate><topic>ACQUISITION RADAR</topic><topic>AERODYNAMIC HEATING</topic><topic>APOGEE</topic><topic>DESCENT TRAJECTORIES</topic><topic>FLIGHT TESTING</topic><topic>FLUID DYNAMICS</topic><topic>GROUND SUPPORT EQUIPMENT</topic><topic>GUIDED MISSILE LAUNCHERS</topic><topic>GUIDED MISSILE RANGES</topic><topic>IMPACT PREDICTION</topic><topic>METEOROLOGICAL BALLOONS</topic><topic>METEOROLOGICAL PHENOMENA</topic><topic>Meteorology</topic><topic>PERFORMANCE(ENGINEERING)</topic><topic>RADAR BEACONS</topic><topic>RADAR CONFUSION REFLECTORS</topic><topic>RADAR TRACKING</topic><topic>Rockets</topic><topic>SOLID PROPELLANT ROCKET ENGINES</topic><topic>SOUNDING ROCKETS</topic><topic>TELEMETER SYSTEMS</topic><topic>UPPER ATMOSPHERE</topic><topic>VIPER ROCKETS</topic><toplevel>online_resources</toplevel><creatorcontrib>Bollermann,Bruce</creatorcontrib><creatorcontrib>Walker,Robert L</creatorcontrib><creatorcontrib>SPACE DATA CORP PHOENIX ARIZ</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Bollermann,Bruce</au><au>Walker,Robert L</au><aucorp>SPACE DATA CORP PHOENIX ARIZ</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>DESIGN, DEVELOPMENT AND FLIGHT TEST OF THE VIPER DART ROBIN METEOROLOGICAL ROCKET SYSTEM</btitle><date>1968-06-30</date><risdate>1968</risdate><abstract>The Viper Dart Robin Meteorological Rocket System has been developed to obtain high altitude density and wind data by utilizing the Robin inflatable sphere as a sensing device. The system consists of a rocket motor, an unpowered dart, and the Robin inflatable sphere. Flight tests of the system provided density, temperature, pressure and wind data from an altitude of about 90 kilometers to an altitude of approximately 40 kilometers or less. (Author)</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng |
recordid | cdi_dtic_stinet_AD0675608 |
source | DTIC Technical Reports |
subjects | ACQUISITION RADAR AERODYNAMIC HEATING APOGEE DESCENT TRAJECTORIES FLIGHT TESTING FLUID DYNAMICS GROUND SUPPORT EQUIPMENT GUIDED MISSILE LAUNCHERS GUIDED MISSILE RANGES IMPACT PREDICTION METEOROLOGICAL BALLOONS METEOROLOGICAL PHENOMENA Meteorology PERFORMANCE(ENGINEERING) RADAR BEACONS RADAR CONFUSION REFLECTORS RADAR TRACKING Rockets SOLID PROPELLANT ROCKET ENGINES SOUNDING ROCKETS TELEMETER SYSTEMS UPPER ATMOSPHERE VIPER ROCKETS |
title | DESIGN, DEVELOPMENT AND FLIGHT TEST OF THE VIPER DART ROBIN METEOROLOGICAL ROCKET SYSTEM |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-15T20%3A17%3A05IST&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=DESIGN,%20DEVELOPMENT%20AND%20FLIGHT%20TEST%20OF%20THE%20VIPER%20DART%20ROBIN%20METEOROLOGICAL%20ROCKET%20SYSTEM&rft.au=Bollermann,Bruce&rft.aucorp=SPACE%20DATA%20CORP%20PHOENIX%20ARIZ&rft.date=1968-06-30&rft_id=info:doi/&rft_dat=%3Cdtic_1RU%3EAD0675608%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 |