KVD-1
KVD-1 was an upper stage LOX/LH2 cryogenic engine developed by Isayev Design Bureau (now KB KhIMMASH) of Russia in early 1960s. It is a modified version of RD-56 which was developed with an intention to manufacture cryogenic engine for upper stage of Lunar N-1 launch vehicle. It was to be used in USSR moon missions. KVD-1 can produce engine thrust of 7.5 tonnes.
primaryTopic
KVD-1
KVD-1 was an upper stage LOX/LH2 cryogenic engine developed by Isayev Design Bureau (now KB KhIMMASH) of Russia in early 1960s. It is a modified version of RD-56 which was developed with an intention to manufacture cryogenic engine for upper stage of Lunar N-1 launch vehicle. It was to be used in USSR moon missions. KVD-1 can produce engine thrust of 7.5 tonnes.
has abstract
KVD-1 was an upper stage LOX/L ...... e engine thrust of 7.5 tonnes.
@en
KVD-1はソビエト連邦のイサーエフ設計局(現在の A.M. ...... 素を推進剤とする上段エンジンと比較しても遜色ない水準である。
@ja
Le KVD-1 était un moteur cryog ...... ait une poussée de 7,5 tonnes.
@fr
RD-56是苏联第一款液氢液氧火箭发动机，世界上第一款高压补 ...... 20也都采用了这种结构，成为了一种苏联特色的氢氧发动机设计。
@zh
Link from a Wikipage to an external page
Wikipage page ID
41,571,990
Wikipage revision ID
741,589,429
associated
burn time
combustion chamber
Cycle
date
first date
2001-04-20
fuel
gimbal
None; uses 2 vernier engines for attitude control
last date
2010-12-25
mixture ratio
oxidiser
purpose
Upper stage engine
reason
not doubting the engine was de ...... a lot of unverifiable claims.
specific impulse vacuum
subject
hypernym
comment
KVD-1 was an upper stage LOX/L ...... e engine thrust of 7.5 tonnes.
@en
KVD-1はソビエト連邦のイサーエフ設計局(現在の A.M. ...... 素を推進剤とする上段エンジンと比較しても遜色ない水準である。
@ja
Le KVD-1 était un moteur cryog ...... ait une poussée de 7,5 tonnes.
@fr
RD-56是苏联第一款液氢液氧火箭发动机，世界上第一款高压补 ...... 20也都采用了这种结构，成为了一种苏联特色的氢氧发动机设计。
@zh
label
KVD-1
@en
KVD-1
@fr
KVD-1
@ja
RD-56
@zh