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Statements

Subject Item
dbr:Hughes_JB-3_Tiamat
rdf:type
dbo:Weapon schema:Product wikidata:Q728 owl:Thing dbo:Device
rdfs:label
JB-3 Tiamat Hughes JB-3 Tiamat Hughes JB-3 Tiamat
rdfs:comment
The JB-3 Tiamat was subsonic air-to-air missile program that began in January 1944 for the U.S. Army Air Force under project MX-570. Prime contractor was Hughes Aircraft Company Electronics Division which developed the Tiamat with the assistance of the National Advisory Committee for Aeronautics, (NACA). Tiamat was propelled by a rocket motor of a boost-sustain dual-thrust type, providing 7,200 lbf (32 kN) of thrust for 3.5 seconds, followed by 200 lbf (0.89 kN) for 45 seconds of cruising flight at 600 miles per hour (970 km/h). Tiamat used semi-active radar homing radar guidance to intercept the target aircraft, with a proximity fuze to detonate the missile's 100 lb (45 kg) High Explosive warhead when within lethal range of an enemy aircraft. The JB-3 program was quickly reduced in status Хьюз JB-3 Тиамат (англ. Tiamat) — управляемая ракета «воздух-воздух», разработанная ВВС США во время Второй Мировой войны. Первая созданная в США управляемая ракета «воздух-воздух». Разработка ракеты продолжалась до 1947 года, но была остановлена в связи с моральным устареванием снаряда. Il JB-3 Tiamat, anche noto come MX-570, è stato uno dei primi missili aria-aria sviluppato dalla Hughes Aircraft Company per la United States Army Air Forces durante la Seconda Guerra Mondiale. Considerato come un veicolo puramente sperimentale, i suoi test di lancio vennero effettuati per diversi anni prima che il progetto venisse chiuso definitivamente.
foaf:name
JB-3 Tiamat
dbp:name
JB-3 Tiamat
foaf:depiction
n19:JB-3_Tiamat.jpg
dcterms:subject
dbc:World_War_II_guided_missiles_of_the_United_States dbc:Hughes_Aircraft_Company dbc:Weapons_and_ammunition_introduced_in_1945
dbo:wikiPageID
51778460
dbo:wikiPageRevisionID
1112363196
dbo:wikiPageWikiLink
dbr:Robert_R._Gilruth dbr:Hughes_Aircraft_Company dbc:World_War_II_guided_missiles_of_the_United_States dbr:U.S._Army_Air_Force dbr:Semi-active_radar_homing dbr:Wright_Field dbr:Langley_Field dbc:Hughes_Aircraft_Company dbr:NACA dbr:Air_Materiel_Command dbr:AAM-A-1_Firebird dbr:Robert_Thomas_Jones_(engineer) dbr:Air-to-air_missile dbr:AIM-4_Falcon dbr:GAR-1_Falcon dbr:Enola_Gay dbr:United_States_Air_Force dbc:Weapons_and_ammunition_introduced_in_1945 dbr:Proximity_fuze dbr:National_Advisory_Committee_for_Aeronautics dbr:Monsanto dbr:Paul_Tibbets dbr:Douglas_A-26_Invader dbr:Wendover_Field dbr:Eglin_Field
owl:sameAs
dbpedia-it:JB-3_Tiamat yago-res:Hughes_JB-3_Tiamat dbpedia-ru:Hughes_JB-3_Tiamat wikidata:Q4040820 n20:3kTFK
dbp:wikiPageUsesTemplate
dbt:Infobox_weapon dbt:USAF_early_missiles dbt:Cite_book dbt:Use_dmy_dates dbt:Refbegin dbt:Reflist dbt:Convert dbt:Refend
dbo:thumbnail
n19:JB-3_Tiamat.jpg?width=300
dbp:designDate
1944
dbp:designer
dbr:NACA dbr:Hughes_Aircraft_Company
dbp:engine
Rocket
dbp:filling
HE
dbp:imageSize
300
dbp:isExplosive
yes
dbp:isMissile
yes
dbp:launchPlatform
dbr:Douglas_A-26_Invader
dbp:manufacturer
dbr:Hughes_Aircraft_Company
dbp:number
35
dbp:origin
United States
dbp:productionDate
1945
dbp:service
1945
dbp:type
dbr:Air-to-air_missile
dbp:usedBy
dbr:United_States_Air_Force
dbo:abstract
Хьюз JB-3 Тиамат (англ. Tiamat) — управляемая ракета «воздух-воздух», разработанная ВВС США во время Второй Мировой войны. Первая созданная в США управляемая ракета «воздух-воздух». Разработка ракеты продолжалась до 1947 года, но была остановлена в связи с моральным устареванием снаряда. The JB-3 Tiamat was subsonic air-to-air missile program that began in January 1944 for the U.S. Army Air Force under project MX-570. Prime contractor was Hughes Aircraft Company Electronics Division which developed the Tiamat with the assistance of the National Advisory Committee for Aeronautics, (NACA). Tiamat was propelled by a rocket motor of a boost-sustain dual-thrust type, providing 7,200 lbf (32 kN) of thrust for 3.5 seconds, followed by 200 lbf (0.89 kN) for 45 seconds of cruising flight at 600 miles per hour (970 km/h). Tiamat used semi-active radar homing radar guidance to intercept the target aircraft, with a proximity fuze to detonate the missile's 100 lb (45 kg) High Explosive warhead when within lethal range of an enemy aircraft. The JB-3 program was quickly reduced in status following the end of WWII. Testing by the NACA and US Army Air Force continued into 1946. Though the project was cancelled due to ongoing problems, missiles already under construction were used by the National Advisory Committee for Aeronautics for research during the next few years. During the program considerable research was conducted including a radical modification to the aerodynamic design testing swept wings. Existing during a period from where anything was tried, to limited development funding, the JB-3 had proven the limits of existing technology as well as providing much experience. With the appearance of more promising missile designs the JB-3 had gone from the cutting edge of technology to obsolete in just a few years time. Il JB-3 Tiamat, anche noto come MX-570, è stato uno dei primi missili aria-aria sviluppato dalla Hughes Aircraft Company per la United States Army Air Forces durante la Seconda Guerra Mondiale. Considerato come un veicolo puramente sperimentale, i suoi test di lancio vennero effettuati per diversi anni prima che il progetto venisse chiuso definitivamente. Il progetto Tiamat ebbe inizio nel gennaio 1944 quando venne firmato un contratto tra la Hughes Aircraft e l'USAAF per lo sviluppo di un missile aria-aria sperimentale subsonico a propellente solido. Sviluppato in cooperazione con la National Advisory Committee for Aeronautics, il Tiamat era un ampio missile a forma di freccia di lunghezza 4,37 metri e di 270 kg di peso.
dbp:guidance
Semi-Active Radar Homing
prov:wasDerivedFrom
wikipedia-en:Hughes_JB-3_Tiamat?oldid=1112363196&ns=0
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283.5
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dbr:Air-to-air_missile
foaf:isPrimaryTopicOf
wikipedia-en:Hughes_JB-3_Tiamat