KDU-414

The KDU-414, is a pressure-fed liquid rocket Propulsion Unit developed and produced by the Isayev Design Bureau. From 1960 onward, it powered several unmanned Soviet Spacecraft, including the first series of Molniya satellites, several Kosmos satellites as well as the space probes Mars 1, Venera 1, Zond 2 and Zond 3, featured as a part of standardized spacecraft buses known as KAUR-2, 2MV and 3MV.

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1960 — 1974  Wikimedia, Wikidata
length 1.02 metre, diameter 0.74 metre, mass 61 kilogram, specific impulse by weight 272 second, maximum thrust 1.96 kilonewton, 
pressure-fed engine, liquid propellant rocket engine, A.M. Isayev Chemical Engineering Design Bureau, Soviet Union, 
Tarshish, 1960s, liquid propellant rocket engine, Republic of Haiti, 1960, pressure-fed engine, Ekran, Dong Fang Hong 2, A.M. Isayev Chemical Engineering Design Bureau, Ashkenaz, Sikh Confederacy, Persia, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Chinland, Calvinist Republic of Ghent, 

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Location: KML, Cluster Map, Maps,

Frameless

Russian thruster2

Type	Subtype	Date	Description	Notes	Source
commons	image		Russian thruster2		Commons