Bristol Siddeley Gamma (original) (raw)
- The Armstrong Siddeley, later Bristol Siddeley Gamma was a family of rocket engines used in British rocketry, including the Black Knight and Black Arrow launch vehicles. They burned kerosene fuel and hydrogen peroxide. Their construction was based on a common combustion chamber design, used either singly or in clusters of up to eight. They were developed by Armstrong Siddeley in Coventry, which later became Bristol Siddeley in 1959, and finally Rolls-Royce in 1966. Engine static testing was carried out at High Down Rocket Test Site, near The Needles on the Isle of Wight (50°39′38.90″N 1°34′38.25″W / 50.6608056°N 1.5772917°W). (Spadeadam in Cumbria wasn't used for testing until Blue Streak, after Gamma). (en)
- Armstrong Siddeley, kemudian Bristol Siddeley Gamma adalah keluarga dari sebuah mesin roket yang digunakan dalam peroketan Inggris, termasuk kendaraan peluncuran Black Knight dan Black Arrow. Mereka membakar bahan bakar minyak tanah dan hidrogen peroksida. Keluarga mesin itu didasarkan pada desain ruang bakar umum, digunakan baik sendiri atau dalam kelompok hingga delapan. Mereka dikembangkan oleh Armstrong-Siddeley di Coventry, yang kemudian menjadi Bristol Siddeley pada tahun 1959, dan akhirnya Rolls-Royce pada tahun 1966. (in)
- 16828595 (xsd:integer)
- 16858 (xsd:nonNegativeInteger)
- 1084018484 (xsd:integer)
- dbr:Rolls-Royce_Limited
- dbr:Black_Arrow
- dbr:Black_Knight_(rocket)
- dbr:Blue_Steel_(missile)
- dbr:Hydrogen_peroxide
- dbr:Coventry
- dbr:Armstrong_Siddeley
- dbc:Armstrong_Siddeley_aircraft_engines
- dbc:Bristol_Siddeley_aircraft_engines
- dbc:Rocket_engines_using_hot_cycle_hydrogen_peroxide_propellant
- dbr:Bristol_Siddeley
- dbr:Ballistic_missile
- dbr:Blue_Streak_missile
- dbr:Isle_of_Wight
- dbr:Armstrong_Siddeley_Stentor
- dbc:Rocket_engines_using_the_staged_combustion_cycle
- dbr:Larch_(rocket_engine)
- dbr:High-test_peroxide
- dbr:High_Down_Rocket_Test_Site
- dbr:The_Needles
- dbr:Staged_combustion_cycle_(rocket)
- dbr:Hypergolic
- dbr:RAF_Spadeadam
- dbr:RP-1
- dbr:Regenerative_cooling_(rocket)
- dbr:Woomera_Test_Range
- dbr:Cuckoo_(Rocket_motor)
- dbr:Stentor_(Rocket_engine)
- dbr:Bristol-Siddeley
- dbr:Gamma_201
- dbr:Gamma_301
- dbr:Gamma_8
- dbr:High_Down_(Rocketry_test_site)
- dbr:LR-40_(Rocket_engine)
- dbr:Project_Dazzle
- 120.0 (dbd:second)
- 125.0 (dbd:second)
- -120.0 (dbd:second)
- Black Knight tail showing engines (en)
- Gamma 2 rocket engine, used for the second stage (en)
- Gamma 8 rocket engine on Black Arrow 1st stage (en)
- 2 (xsd:integer)
- 4 (xsd:integer)
- 8 (xsd:integer)
- Britain (en)
- kerosene (en)
- 8 (xsd:integer)
- Gamma 2 (en)
- Gamma 201 (en)
- Gamma 301 (en)
- Gamma 8 (en)
- Hydrogen peroxide (en)
- 1 (xsd:integer)
- 2 (xsd:integer)
- float: left; font-size: 95%; width: 25em; margin: 0 2em 2em 0; (en)
- - (en)
- 0.680000 (xsd:double)
- liquid (en)
- dbt:BristolAeroengines
- dbt:ASaeroengines
- dbt:Commons_category
- dbt:Convert
- dbt:Coord
- dbt:EngvarB
- dbt:Expand_section
- dbt:Infobox_rocket_engine
- dbt:Reflist
- dbt:Rocket_engines
- dbt:Sfnp
- dbt:Short_description
- dbt:Use_dmy_dates
- dbc:Armstrong_Siddeley_aircraft_engines
- dbc:Bristol_Siddeley_aircraft_engines
- dbc:Rocket_engines_using_hot_cycle_hydrogen_peroxide_propellant
- dbc:Rocket_engines_using_the_staged_combustion_cycle
- 50.660805555555555 -1.5772916666666668
- yago:WikicatArmstrongSiddeleyAircraftEngines
- yago:WikicatBristolSiddeleyAircraftEngines
- geo:SpatialThing
- yago:WikicatRocketEngines
- yago:WikicatRocketEnginesUsingKerosenePropellant
- yago:AircraftEngine102687423
- yago:Artifact100021939
- yago:Device103183080
- yago:Engine103287733
- yago:Instrumentality103575240
- yago:JetEngine103596285
- yago:Machine103699975
- yago:Motor103789946
- yago:Object100002684
- yago:PhysicalEntity100001930
- yago:Reaction-propulsionEngine104057435
- yago:Rocket104099175
- yago:Whole100003553
- Armstrong Siddeley, kemudian Bristol Siddeley Gamma adalah keluarga dari sebuah mesin roket yang digunakan dalam peroketan Inggris, termasuk kendaraan peluncuran Black Knight dan Black Arrow. Mereka membakar bahan bakar minyak tanah dan hidrogen peroksida. Keluarga mesin itu didasarkan pada desain ruang bakar umum, digunakan baik sendiri atau dalam kelompok hingga delapan. Mereka dikembangkan oleh Armstrong-Siddeley di Coventry, yang kemudian menjadi Bristol Siddeley pada tahun 1959, dan akhirnya Rolls-Royce pada tahun 1966. (in)
- The Armstrong Siddeley, later Bristol Siddeley Gamma was a family of rocket engines used in British rocketry, including the Black Knight and Black Arrow launch vehicles. They burned kerosene fuel and hydrogen peroxide. Their construction was based on a common combustion chamber design, used either singly or in clusters of up to eight. They were developed by Armstrong Siddeley in Coventry, which later became Bristol Siddeley in 1959, and finally Rolls-Royce in 1966. (en)
- Bristol Siddeley Gamma (en)
- Bristol Siddeley Gamma (in)
- freebase:Bristol Siddeley Gamma
- yago-res:Bristol Siddeley Gamma
- wikidata:Bristol Siddeley Gamma
- dbpedia-id:Bristol Siddeley Gamma
- https://global.dbpedia.org/id/4c78Q
- POINT(-1.5772916078568 50.660804748535)
- 50.660805 (xsd:float)
- -1.577292 (xsd:float)
- wiki-commons:Special:FilePath/Black_Arrow_R3_Stage_1.jpg
- wiki-commons:Special:FilePath/Black_Knight_Gamma_201_engine_and_re-entry_head.jpg
- wiki-commons:Special:FilePath/Black_Knight_tail.jpg
- wiki-commons:Special:FilePath/Gamma_2_engine.jpg
- wiki-commons:Special:FilePath/Gamma_2_rocket_engine_on_Black_Arrow_2nd_stage.jpg
- wiki-commons:Special:FilePath/Gamma_8_rocket_engine_on_Black_Arrow_1st_stage.jpg
is dbo:wikiPageDisambiguates of
is dbo:wikiPageRedirects of
- dbr:Gamma_(Rocket_engine)
- dbr:Gamma_201
- dbr:Gamma_301
- dbr:Gamma_8
- dbr:Armstrong_Siddeley_Gamma
- dbr:Bristol_Siddeley_Gamma_201
- dbr:Bristol_Siddeley_Gamma_301
- dbr:Bristol_Siddeley_Gamma_Mk.201
- dbr:Bristol_Siddeley_Gamma_Mk.301
is dbo:wikiPageWikiLink of
- dbr:List_of_aircraft_engines
- dbr:Black_Arrow
- dbr:Black_Knight_(rocket)
- dbr:De_Havilland_Sprite
- dbr:Gamma_(disambiguation)
- dbr:List_of_rocket_stages
- dbr:Comparison_of_orbital_rocket_engines
- dbr:Napier_Scorpion
- dbr:Gamma_(Rocket_engine)
- dbr:Gamma_201
- dbr:Gamma_301
- dbr:Gamma_8
- dbr:Armstrong_Siddeley_Gamma
- dbr:Bristol_Siddeley_Gamma_201
- dbr:Bristol_Siddeley_Gamma_301
- dbr:Bristol_Siddeley_Gamma_Mk.201
- dbr:Bristol_Siddeley_Gamma_Mk.301
is foaf:primaryTopic of