About: Armstrong Siddeley Stentor

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The Armstrong Siddeley Stentor, latterly Bristol Siddeley BSSt.1 Stentor, was a two-chamber HTP rocket engine used to power the Blue Steel stand-off missile carried by Britain's V bomber force. The high thrust chamber was used for the first 29 seconds, after which it was shut down and a smaller cruise chamber was used for the rest of the powered flight.

Attributes	Values
rdf:type	software yago:WikicatArmstrongSiddeleyRocketEngines yago:WikicatRocketEnginesUsingKerosenePropellant 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
rdfs:label	Armstrong Siddeley Stentor (de) Armstrong Siddeley Stentor (en) Armstrong Siddeley Stentor (in) アームストロング・シドレーステンター (ja)
rdfs:comment	The Armstrong Siddeley Stentor, latterly Bristol Siddeley BSSt.1 Stentor, was a two-chamber HTP rocket engine used to power the Blue Steel stand-off missile carried by Britain's V bomber force. The high thrust chamber was used for the first 29 seconds, after which it was shut down and a smaller cruise chamber was used for the rest of the powered flight. (en) Der Armstrong Siddeley Stentor, später auch Bristol Siddeley BSSt.1 Stentor war ein zweistufiges Raketentriebwerk, das der britische Hersteller Armstrong Siddeley ab 1960 baute. Es diente dem Antrieb der Lenkflugkörpers Avro Blue Steel, die von der britischen V-Bomberflotte genutzt wurden. Eine Brennkammer lieferte den Startschub und wurde 29 sec. nach dem Abschuss abgestellt. Die zweite, kleinere Brennkammer wurde für den Rest des Fluges genutzt. (de) Armstrong Siddeley Stentor, ditulis Bristol Siddeley BSSt.1 Stentor, adalah sebuah mesin roket dua-ruang yang digunakan untuk menyalakan rudal stand-off Blue Steel yang dilakukan dengan angkatan pengebom V Inggris. Satu ruang digunakan untuk peningkatkan awal, kemudian, 29 detik setelah melepaskan dorongan ruang ditutup dan ruang pesiar yang lebih kecil digunakan untuk sebagian besar penerbangan. Mesin itu didorong oleh kimia propelan hidrogen peroksida / minyak tanah. (in) アームストロング・シドレーステンター（Armstrong Siddeley Stentor）, 後にブリストル・シドレー BSSt.1 ステンターはブルースティールミサイル用のロケットエンジンである。 (ja)
foaf:depiction
dcterms:subject	Armstrong Siddeley rocket engines Rocket engines using hot cycle hydrogen peroxide propellant Rocket engines using kerosene propellant
Wikipage page ID	16954112 (xsd:integer)
Wikipage revision ID	1004519104 (xsd:integer)
Link from a Wikipage to another Wikipage	List of aircraft engines Blue Steel (missile) United Kingdom University of Liverpool Armstrong Siddeley Armstrong Siddeley rocket engines Rocket engines using hot cycle hydrogen peroxide propellant Cambridge Science Centre Liquid-propellant rocket Blue Steel missile Royal Air Force Museum Cosford Rocket engines using kerosene propellant High-test peroxide Newark Air Museum Midland Air Museum Rocket engine V bomber South Yorkshire Aircraft Museum Gamma (Rocket engine) Bristol Siddeley BS.605
sameAs	Armstrong Siddeley Stentor Armstrong Siddeley Stentor Armstrong Siddeley Stentor Armstrong Siddeley Stentor Armstrong Siddeley Stentor Armstrong Siddeley Stentor Armstrong Siddeley Stentor Armstrong Siddeley Stentor
specfuelcon	Specific impulse: ~ (en)
thrust	large boost chamber rated at (en) smaller cruise chamber rated at (en)
dbp:wikiPageUsesTemplate	dbt:Armstrong_Siddeley_aeroengines dbt:Bristol_aeroengines dbt:Rocketspecs dbt:Commons_category dbt:Convert dbt:Reflist dbt:Rocket_engines dbt:Short_description dbt:Use_British_English dbt:Use_dmy_dates dbt:Aircontent dbt:Infobox_aircraft_engine
thumbnail	wiki-commons:Special:FilePath/AS_Stentor_RRHT.jpg?width=300
national origin	United Kingdom
diameter	wide, high (en)
manufacturer	Armstrong Siddeley
oxidiser	hydrogen peroxide (en)
related	*Bristol Siddeley BS.605 (en)
type	Liquid-propellant rocket Rocket engine
weight	including oil and nitrogen (en)
has abstract	The Armstrong Siddeley Stentor, latterly Bristol Siddeley BSSt.1 Stentor, was a two-chamber HTP rocket engine used to power the Blue Steel stand-off missile carried by Britain's V bomber force. The high thrust chamber was used for the first 29 seconds, after which it was shut down and a smaller cruise chamber was used for the rest of the powered flight. (en) Der Armstrong Siddeley Stentor, später auch Bristol Siddeley BSSt.1 Stentor war ein zweistufiges Raketentriebwerk, das der britische Hersteller Armstrong Siddeley ab 1960 baute. Es diente dem Antrieb der Lenkflugkörpers Avro Blue Steel, die von der britischen V-Bomberflotte genutzt wurden. Eine Brennkammer lieferte den Startschub und wurde 29 sec. nach dem Abschuss abgestellt. Die zweite, kleinere Brennkammer wurde für den Rest des Fluges genutzt. (de) Armstrong Siddeley Stentor, ditulis Bristol Siddeley BSSt.1 Stentor, adalah sebuah mesin roket dua-ruang yang digunakan untuk menyalakan rudal stand-off Blue Steel yang dilakukan dengan angkatan pengebom V Inggris. Satu ruang digunakan untuk peningkatkan awal, kemudian, 29 detik setelah melepaskan dorongan ruang ditutup dan ruang pesiar yang lebih kecil digunakan untuk sebagian besar penerbangan. Mesin itu didorong oleh kimia propelan hidrogen peroksida / minyak tanah. (in) アームストロング・シドレーステンター（Armstrong Siddeley Stentor）, 後にブリストル・シドレー BSSt.1 ステンターはブルースティールミサイル用のロケットエンジンである。 (ja)
first run	c.1960 (en)
fueltype	kerosene (en)
lists	*List of aircraft engines (en)
major applications	Blue Steel (missile)
gold:hypernym	Engine
prov:wasDerivedFrom	wikipedia-en:Armstrong_Siddeley_Stentor?oldid=1004519104&ns=0
page length (characters) of wiki page	5714 (xsd:nonNegativeInteger)
foaf:isPrimaryTopicOf	wikipedia-en:Armstrong_Siddeley_Stentor
is Link from a Wikipage to another Wikipage of	List of aircraft engines Blue Steel (missile) Armstrong Siddeley Stentor (disambiguation) Bristol Siddeley 605

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