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Proton / UR-500 K/D

Proton / UR-500 K/D

Proton / UR-500 family · built by Russian Federal Space Agency (ROSCOSMOS) · maiden flight 1967-03-10

Profile data last updated: 2026-08-29T15:37:07.354998+00:00 | 7531-10-17

This four stage version of the Proton was originally designed to send manned circumlunar spacecraft into translunar trajectory.

Specifications

57.0 mLength
4.0 mDiameter
696 tLaunch mass
4Stages
8847 kNLiftoff thrust

Payload Capacity

No payload capacity figures published for this configuration.

Lifetime Launch Record

As reported by Launch Library 2 across this rocket's entire history, not just the launches tracked on this site.

39Total launches
24Successful
15Failed
0Upcoming

Launches Tracked on This Site

39In our archive
61.5%Success rate
Mar 10, 1967 11:30 UTCEarliest tracked
Jun 14, 1975 03:00 UTCMost recent
MissionDateStatus
Proton | Venera-10 Jun 14, 1975 03:00 UTC Success
Proton | Venera-9 Jun 08, 1975 02:38 UTC Success
Proton | Luna-23 Oct 28, 1974 14:30 UTC Success
Proton | Luna-22 May 29, 1974 08:56 UTC Success
Proton | Mars-7 Aug 09, 1973 17:00 UTC Success
Proton | Mars-6 Aug 05, 1973 17:45 UTC Success
Proton | Mars-5 Jul 25, 1973 18:55 UTC Success
Proton | Mars-4 Jul 21, 1973 19:30 UTC Success
Proton | Luna-21 Jan 08, 1973 06:55 UTC Success
Proton | Luna-20 Feb 14, 1972 03:27 UTC Success
Proton | Luna-19 Sep 28, 1971 10:00 UTC Success
Proton | Luna-18 Sep 02, 1971 13:40 UTC Success
Proton | Mars-3 May 28, 1971 15:26 UTC Success
Proton | Mars-2 May 19, 1971 16:22 UTC Success
Proton | Mars-2d May 10, 1971 16:58 UTC Failure

Wikipedia