Test launch control equipment for small solid rockets or target projectiles

The utility model provides test launch control equipment for a small solid rocket or a target projectile, belongs to the technical field of test launch control, and solves the problems of complex structure, larger size, higher cost and poorer universality of the existing equipment. The device compri...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: CHEN JINGPENG, ZHAO XINQIANG, LIU PENG, LIU KUIFANG, LIANG JIANJUN, LIU KAI, SU PENG
Format: Patent
Sprache:chi ; 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 CHEN JINGPENG
ZHAO XINQIANG
LIU PENG
LIU KUIFANG
LIANG JIANJUN
LIU KAI
SU PENG
description The utility model provides test launch control equipment for a small solid rocket or a target projectile, belongs to the technical field of test launch control, and solves the problems of complex structure, larger size, higher cost and poorer universality of the existing equipment. The device comprises a test launch control shell, and a main control computer, a keyboard-mouse-display all-in-one machine, a distribution box and a photoelectric converter which are integrated in the shell. Test launch control software is configured on the main control computer, a data input end of the test launch control software is connected with a data sensor carried on the rocket or the target missile to be tested, a data output end of the test launch control software is connected with the keyboard-mouse-display all-in-one machine and is accessed to a local area network through a photoelectric converter, and a control signal output end of the test launch control software is connected with electrical equipment on the rocket or
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN217821328UU</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN217821328UU</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN217821328UU3</originalsourceid><addsrcrecordid>eNqNyjEKwkAQRuE0FqLeYbC3yKYwfVAEwSqpw7L-0cTJzrozub8WHsDqwcdbF9cWasR-ieFJQaJlYcJ7GdOMaDRIJp09M6nweKcs4QVT-rL5_IBRyjIh2MjQbbEaPCt2v26K_fnUNpcDkvTQ5AMirG9urjzWrqxc3XXVX9MHBrU2wA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Test launch control equipment for small solid rockets or target projectiles</title><source>esp@cenet</source><creator>CHEN JINGPENG ; ZHAO XINQIANG ; LIU PENG ; LIU KUIFANG ; LIANG JIANJUN ; LIU KAI ; SU PENG</creator><creatorcontrib>CHEN JINGPENG ; ZHAO XINQIANG ; LIU PENG ; LIU KUIFANG ; LIANG JIANJUN ; LIU KAI ; SU PENG</creatorcontrib><description>The utility model provides test launch control equipment for a small solid rocket or a target projectile, belongs to the technical field of test launch control, and solves the problems of complex structure, larger size, higher cost and poorer universality of the existing equipment. The device comprises a test launch control shell, and a main control computer, a keyboard-mouse-display all-in-one machine, a distribution box and a photoelectric converter which are integrated in the shell. Test launch control software is configured on the main control computer, a data input end of the test launch control software is connected with a data sensor carried on the rocket or the target missile to be tested, a data output end of the test launch control software is connected with the keyboard-mouse-display all-in-one machine and is accessed to a local area network through a photoelectric converter, and a control signal output end of the test launch control software is connected with electrical equipment on the rocket or</description><language>chi ; eng</language><subject>CONTROL OR REGULATING SYSTEMS IN GENERAL ; CONTROLLING ; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS ; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS ; PHYSICS ; REGULATING</subject><creationdate>2022</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20221115&amp;DB=EPODOC&amp;CC=CN&amp;NR=217821328U$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20221115&amp;DB=EPODOC&amp;CC=CN&amp;NR=217821328U$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>CHEN JINGPENG</creatorcontrib><creatorcontrib>ZHAO XINQIANG</creatorcontrib><creatorcontrib>LIU PENG</creatorcontrib><creatorcontrib>LIU KUIFANG</creatorcontrib><creatorcontrib>LIANG JIANJUN</creatorcontrib><creatorcontrib>LIU KAI</creatorcontrib><creatorcontrib>SU PENG</creatorcontrib><title>Test launch control equipment for small solid rockets or target projectiles</title><description>The utility model provides test launch control equipment for a small solid rocket or a target projectile, belongs to the technical field of test launch control, and solves the problems of complex structure, larger size, higher cost and poorer universality of the existing equipment. The device comprises a test launch control shell, and a main control computer, a keyboard-mouse-display all-in-one machine, a distribution box and a photoelectric converter which are integrated in the shell. Test launch control software is configured on the main control computer, a data input end of the test launch control software is connected with a data sensor carried on the rocket or the target missile to be tested, a data output end of the test launch control software is connected with the keyboard-mouse-display all-in-one machine and is accessed to a local area network through a photoelectric converter, and a control signal output end of the test launch control software is connected with electrical equipment on the rocket or</description><subject>CONTROL OR REGULATING SYSTEMS IN GENERAL</subject><subject>CONTROLLING</subject><subject>FUNCTIONAL ELEMENTS OF SUCH SYSTEMS</subject><subject>MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS</subject><subject>PHYSICS</subject><subject>REGULATING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNyjEKwkAQRuE0FqLeYbC3yKYwfVAEwSqpw7L-0cTJzrozub8WHsDqwcdbF9cWasR-ieFJQaJlYcJ7GdOMaDRIJp09M6nweKcs4QVT-rL5_IBRyjIh2MjQbbEaPCt2v26K_fnUNpcDkvTQ5AMirG9urjzWrqxc3XXVX9MHBrU2wA</recordid><startdate>20221115</startdate><enddate>20221115</enddate><creator>CHEN JINGPENG</creator><creator>ZHAO XINQIANG</creator><creator>LIU PENG</creator><creator>LIU KUIFANG</creator><creator>LIANG JIANJUN</creator><creator>LIU KAI</creator><creator>SU PENG</creator><scope>EVB</scope></search><sort><creationdate>20221115</creationdate><title>Test launch control equipment for small solid rockets or target projectiles</title><author>CHEN JINGPENG ; ZHAO XINQIANG ; LIU PENG ; LIU KUIFANG ; LIANG JIANJUN ; LIU KAI ; SU PENG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN217821328UU3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2022</creationdate><topic>CONTROL OR REGULATING SYSTEMS IN GENERAL</topic><topic>CONTROLLING</topic><topic>FUNCTIONAL ELEMENTS OF SUCH SYSTEMS</topic><topic>MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS</topic><topic>PHYSICS</topic><topic>REGULATING</topic><toplevel>online_resources</toplevel><creatorcontrib>CHEN JINGPENG</creatorcontrib><creatorcontrib>ZHAO XINQIANG</creatorcontrib><creatorcontrib>LIU PENG</creatorcontrib><creatorcontrib>LIU KUIFANG</creatorcontrib><creatorcontrib>LIANG JIANJUN</creatorcontrib><creatorcontrib>LIU KAI</creatorcontrib><creatorcontrib>SU PENG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>CHEN JINGPENG</au><au>ZHAO XINQIANG</au><au>LIU PENG</au><au>LIU KUIFANG</au><au>LIANG JIANJUN</au><au>LIU KAI</au><au>SU PENG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Test launch control equipment for small solid rockets or target projectiles</title><date>2022-11-15</date><risdate>2022</risdate><abstract>The utility model provides test launch control equipment for a small solid rocket or a target projectile, belongs to the technical field of test launch control, and solves the problems of complex structure, larger size, higher cost and poorer universality of the existing equipment. The device comprises a test launch control shell, and a main control computer, a keyboard-mouse-display all-in-one machine, a distribution box and a photoelectric converter which are integrated in the shell. Test launch control software is configured on the main control computer, a data input end of the test launch control software is connected with a data sensor carried on the rocket or the target missile to be tested, a data output end of the test launch control software is connected with the keyboard-mouse-display all-in-one machine and is accessed to a local area network through a photoelectric converter, and a control signal output end of the test launch control software is connected with electrical equipment on the rocket or</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language chi ; eng
recordid cdi_epo_espacenet_CN217821328UU
source esp@cenet
subjects CONTROL OR REGULATING SYSTEMS IN GENERAL
CONTROLLING
FUNCTIONAL ELEMENTS OF SUCH SYSTEMS
MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS
PHYSICS
REGULATING
title Test launch control equipment for small solid rockets or target projectiles
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-30T01%3A03%3A27IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=CHEN%20JINGPENG&rft.date=2022-11-15&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN217821328UU%3C/epo_EVB%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