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- Grigorovich_TB-5 abstract "Grigorovich TB-5 (Russian: Григорович ТБ-5) was an experimental heavy bomber designed and tested in the Soviet Union in the early 1930s. Designed as a competitor for TB-3, TB-5 was intended to be powered by two FED 24-cylinder X engines of 746 kW (1,000 hp) each. When these were canceled, the underwing pods were revised to each house a pair of Bristol Jupiter engines in a push-pull configuration. Despite projected performance inferior to TB-3, it was hoped that TB-5 would gain an advantage by using less metal (in short supply at the time) thanks to its mixed construction of fabric-covered metal frame.Test flights began on 1 May 1931 with disappointing results, in part due to poor thrust of the rear-facing engines. The prototype TB-5 was wrecked in a crash landing following the in-flight detachment of an engine in Spring 1932, and with the entry into service of the superior TB-3 that year, the TB-5 project was abandoned.".
- Grigorovich_TB-5 designer Grigorovich_(design_bureau).
- Grigorovich_TB-5 origin Soviet_Union.
- Grigorovich_TB-5 thumbnail ТБ-5_на_Центральном_аэродроме.jpg?width=300.
- Grigorovich_TB-5 wikiPageID "19402212".
- Grigorovich_TB-5 wikiPageLength "3840".
- Grigorovich_TB-5 wikiPageOutDegree "16".
- Grigorovich_TB-5 wikiPageRevisionID "668384051".
- Grigorovich_TB-5 wikiPageWikiLink Bristol_Jupiter.
- Grigorovich_TB-5 wikiPageWikiLink Category:Grigorovich_aircraft.
- Grigorovich_TB-5 wikiPageWikiLink Category:Soviet_bomber_aircraft_1930–1939.
- Grigorovich_TB-5 wikiPageWikiLink Farman_F.220.
- Grigorovich_TB-5 wikiPageWikiLink Grigorovich_(design_bureau).
- Grigorovich_TB-5 wikiPageWikiLink PV-1_machine_gun.
- Grigorovich_TB-5 wikiPageWikiLink Push-pull_configuration.
- Grigorovich_TB-5 wikiPageWikiLink Radial_engine.
- Grigorovich_TB-5 wikiPageWikiLink Soviet_Union.
- Grigorovich_TB-5 wikiPageWikiLink Tupolev_TB-3.
- Grigorovich_TB-5 wikiPageWikiLink X_engine.
- Grigorovich_TB-5 wikiPageWikiLink File:ТБ-5_на_Центральном_аэродроме.jpg.
- Grigorovich_TB-5 wikiPageWikiLinkText "Grigorovich TB-5".
- Grigorovich_TB-5 wikiPageWikiLinkText "TB-5".
- Grigorovich_TB-5 wikiPageWikiLinkText "TsKB-8".
- Grigorovich_TB-5 areaAlt "1614.6".
- Grigorovich_TB-5 areaMain "150.0".
- Grigorovich_TB-5 bombs "Up to 2,500 kg of bombs".
- Grigorovich_TB-5 ceilingAlt "8530.0".
- Grigorovich_TB-5 ceilingMain "2,600 m".
- Grigorovich_TB-5 crew "Six".
- Grigorovich_TB-5 designer Grigorovich_(design_bureau).
- Grigorovich_TB-5 emptyWeightAlt "16497.0".
- Grigorovich_TB-5 emptyWeightMain "7483.0".
- Grigorovich_TB-5 engine(prop)_ "Bristol Jupiter V".
- Grigorovich_TB-5 guns "Two turrets, each with 2× 7.62 mm PV-1 machine guns".
- Grigorovich_TB-5 jetOrProp%3F_ "prop".
- Grigorovich_TB-5 lengthAlt "2209.7999999999997".
- Grigorovich_TB-5 lengthMain "22.1 m".
- Grigorovich_TB-5 loadedWeightAlt "27635.0".
- Grigorovich_TB-5 loadedWeightMain "12535.0".
- Grigorovich_TB-5 loadingAlt "17".
- Grigorovich_TB-5 loadingMain "84".
- Grigorovich_TB-5 maxSpeedAlt "97".
- Grigorovich_TB-5 maxSpeedMain "180.0".
- Grigorovich_TB-5 nationalOrigin Soviet_Union.
- Grigorovich_TB-5 numberBuilt "One".
- Grigorovich_TB-5 numberOfProps "4".
- Grigorovich_TB-5 planeOrCopter%3F_ "plane".
- Grigorovich_TB-5 massAlt "0.07".
- Grigorovich_TB-5 massMain "107".
- Grigorovich_TB-5 powerAlt "450.0".
- Grigorovich_TB-5 powerMain "336.0".
- Grigorovich_TB-5 primaryUser Soviet_Union.
- Grigorovich_TB-5 ref "Shavrov 1985".
- Grigorovich_TB-5 similarAircraft "*TB-3 *Farman F.220".
- Grigorovich_TB-5 spanAlt "3098.8".
- Grigorovich_TB-5 spanMain "31 m".
- Grigorovich_TB-5 status "Retired".
- Grigorovich_TB-5 type "Heavy bomber".
- Grigorovich_TB-5 typeOfProp Radial_engine.
- Grigorovich_TB-5 wikiPageUsesTemplate Template:Aircontent.
- Grigorovich_TB-5 wikiPageUsesTemplate Template:Aircraft_specifications.
- Grigorovich_TB-5 wikiPageUsesTemplate Template:Avyear.
- Grigorovich_TB-5 wikiPageUsesTemplate Template:Cite_book.
- Grigorovich_TB-5 wikiPageUsesTemplate Template:Commons_category.
- Grigorovich_TB-5 wikiPageUsesTemplate Template:Grigorovich_aircraft.
- Grigorovich_TB-5 wikiPageUsesTemplate Template:Infobox_Aircraft_Type.
- Grigorovich_TB-5 wikiPageUsesTemplate Template:Lang-ru.
- Grigorovich_TB-5 wikiPageUsesTemplate Template:Reflist.
- Grigorovich_TB-5 wikiPageUsesTemplate Template:Soviet_bomber_aircraft.
- Grigorovich_TB-5 subject Category:Grigorovich_aircraft.
- Grigorovich_TB-5 subject Category:Soviet_bomber_aircraft_1930–1939.
- Grigorovich_TB-5 hypernym Bomber.
- Grigorovich_TB-5 type Aircraft.
- Grigorovich_TB-5 type MeanOfTransportation.
- Grigorovich_TB-5 type Product.
- Grigorovich_TB-5 type DesignedArtifact.
- Grigorovich_TB-5 type Thing.
- Grigorovich_TB-5 type Q11436.
- Grigorovich_TB-5 comment "Grigorovich TB-5 (Russian: Григорович ТБ-5) was an experimental heavy bomber designed and tested in the Soviet Union in the early 1930s. Designed as a competitor for TB-3, TB-5 was intended to be powered by two FED 24-cylinder X engines of 746 kW (1,000 hp) each. When these were canceled, the underwing pods were revised to each house a pair of Bristol Jupiter engines in a push-pull configuration.".
- Grigorovich_TB-5 label "Grigorovich TB-5".
- Grigorovich_TB-5 sameAs Q1546746.
- Grigorovich_TB-5 sameAs Grigorowitsch_TB-5.
- Grigorovich_TB-5 sameAs m.04n5dv8.
- Grigorovich_TB-5 sameAs Grigorovič_TB-5.
- Grigorovich_TB-5 sameAs Grigoroviç_TB-5.
- Grigorovich_TB-5 sameAs Grigorovich_TB-5.
- Grigorovich_TB-5 sameAs Q1546746.
- Grigorovich_TB-5 wasDerivedFrom Grigorovich_TB-5?oldid=668384051.
- Grigorovich_TB-5 depiction ТБ-5_на_Центральном_аэродроме.jpg.
- Grigorovich_TB-5 isPrimaryTopicOf Grigorovich_TB-5.
