KDU-414
From Spacefaring
Q4206320
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.
1960 — 1974
Wikimedia, Wikidata
Corrective Propulsion Unit; KTDU-414; S5.19
length 1.02 metre, diameter 0.74 metre, mass 61 kilogram, specific impulse by weight 272 second, maximum thrust 1.96 kilonewton,
A.M. Isayev Chemical Engineering Design Bureau, Soviet Union,
A.M. Isayev Chemical Engineering Design Bureau, Dong Fang Hong 2, pressure-fed engine, 1960, liquid propellant rocket engine, 1960s,
-
Location: KML, Cluster Map, Maps,
Russian thruster2| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | Russian thruster2 | Commons | ||
