About: NK-15

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The NK-15 (GRAU index 11D51) was a rocket engine designed and built in the late 1960s by the Kuznetsov Design Bureau. The NK designation was derived from the initials of chief designer Nikolay Kuznetsov. The NK-15 was among the most powerful LOX/kerosene rocket engines when it was built, with a high specific impulse and low structural mass. It was intended for the ill-fated Soviet N-1 Moon rocket.

Attributes	Values
rdfs:label	NK-15 (fr) NK-15 (en) НК-15 (ru)
rdfs:comment	The NK-15 (GRAU index 11D51) was a rocket engine designed and built in the late 1960s by the Kuznetsov Design Bureau. The NK designation was derived from the initials of chief designer Nikolay Kuznetsov. The NK-15 was among the most powerful LOX/kerosene rocket engines when it was built, with a high specific impulse and low structural mass. It was intended for the ill-fated Soviet N-1 Moon rocket. (en) НК-15 (11Д51) — жидкостный ракетный двигатель, разработан в 1962-67 годах для первой ступени ракеты-носителя Н1 (30 двигателей) с использованием опыта по ЖРД 8Д717 (связка из четырёх НК-9) и 8Д517 (одиночный НК-9). Дата первого испытания — декабрь 1963 года. Государственные испытания завершены в октябре 1967 года. Первый запуск в составе РН Н1 выполнен в 1969 году, последний — в 1972 году. Компоненты топлива — жидкий кислород и керосин. (ru) Le NK-15 (indice GRAU : 11D51) est un moteur-fusée à ergols liquides, dérivé du NK-9, mis au point par la société Kouznetsov, entre 1962 et 1967, pour le premier étage du lanceur N-1. Il utilisait l'élément LPD 8D717 (groupe de 30 moteurs) pour le premier étage et 8D517 (groupe de 8 moteurs) pour le second. Le premier test a eu lieu en décembre 1963. Le premier lancement de la fusée N-1 a eu lieu en 1969, le dernier en 1972. Ce moteur brûlait un mélange d'oxygène liquide et de kérosène. (fr)
name	NK-15 (en)
dcterms:subject	Rocket engines of the Soviet Union Science and technology in the Soviet Union Rocket engines using kerosene propellant Rocket engines using the staged combustion cycle Soviet lunar program
Wikipage page ID	29852666 (xsd:integer)
Wikipage revision ID	1122060577 (xsd:integer)
Link from a Wikipage to another Wikipage	Encyclopedia Astronautica Kuznetsov Design Bureau Rocket engines of the Soviet Union Comparison of orbital rocket engines N1 (rocket) NK-33 Science and technology in the Soviet Union Liquid oxygen Rocket engines using kerosene propellant Rocket engines using the staged combustion cycle Soviet lunar program Soviet Union RP-1 Specific impulse LOX Turbopump Staged combustion cycle Rocket engine GRAU index
Link from a Wikipage to an external page	http://www.b14643.de/Spacerockets_1/East_Europe_2/N-1/Propulsion/engines.htm https://web.archive.org/web/20161228022648/http:/astronautix.com/n/nk-15.html http://www.lpre.de/sntk/index.htm
sameAs	NK-15 NK-15 NK-15 NK-15
throttle range	50 (xsd:integer)
thrust to weight	137 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Infobox_rocket_engine dbt:Reflist dbt:Rocket_engines dbt:Short_description
country of origin	Soviet Union
cycle	Staged combustion cycle
date	1960.0 (second)
designer	Kuznetsov Design Bureau
fuel	RP-1
oxidiser	Liquid oxygen
purpose	1 (xsd:integer)
successor	NK-33
type	liquid (en)
has abstract	Le NK-15 (indice GRAU : 11D51) est un moteur-fusée à ergols liquides, dérivé du NK-9, mis au point par la société Kouznetsov, entre 1962 et 1967, pour le premier étage du lanceur N-1. Il utilisait l'élément LPD 8D717 (groupe de 30 moteurs) pour le premier étage et 8D517 (groupe de 8 moteurs) pour le second. Le premier test a eu lieu en décembre 1963. Le premier lancement de la fusée N-1 a eu lieu en 1969, le dernier en 1972. Ce moteur brûlait un mélange d'oxygène liquide et de kérosène. Après les quatre premier vols de cette fusée N-1, tous des échecs, le moteur NK-33 qui est une version améliorée permettant de multiples essais de résistance au feu avec une durée de vie augmentée, devait le remplacer dans une version améliorée du lanceur, N1F, mais le programme fut annulé. (fr) The NK-15 (GRAU index 11D51) was a rocket engine designed and built in the late 1960s by the Kuznetsov Design Bureau. The NK designation was derived from the initials of chief designer Nikolay Kuznetsov. The NK-15 was among the most powerful LOX/kerosene rocket engines when it was built, with a high specific impulse and low structural mass. It was intended for the ill-fated Soviet N-1 Moon rocket. (en) НК-15 (11Д51) — жидкостный ракетный двигатель, разработан в 1962-67 годах для первой ступени ракеты-носителя Н1 (30 двигателей) с использованием опыта по ЖРД 8Д717 (связка из четырёх НК-9) и 8Д517 (одиночный НК-9). Дата первого испытания — декабрь 1963 года. Государственные испытания завершены в октябре 1967 года. Первый запуск в составе РН Н1 выполнен в 1969 году, последний — в 1972 году. Компоненты топлива — жидкий кислород и керосин. (ru)
pumps	Turbopump
prov:wasDerivedFrom	wikipedia-en:NK-15?oldid=1122060577&ns=0
page length (characters) of wiki page	3212 (xsd:nonNegativeInteger)
foaf:isPrimaryTopicOf	wikipedia-en:NK-15
is Link from a Wikipage to another Wikipage of	Kuznetsov Design Bureau N1 (rocket) NK-33 Nikolai Dmitriyevich Kuznetsov JSC Kuznetsov Sergei Korolev Staged combustion cycle Rocket engine
is foaf:primaryTopic of	wikipedia-en:NK-15

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