Proton / UR-500·Russian Federal Space Agency (ROSCOSMOS)
Proton-M Briz-M
active
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Specifications
- Status
- active
- Height
- 53 m
- Diameter
- 7.4 m
- Mass
- 712,000 kg
- Stages
- 4
- Thrust
- 10,000 kN
- Payload to LEO
- 21,000 kg
- Payload to GTO
- 4,500 kg
- First flight
- 2001-04-07
- Total launches
- 68
- Success / Fail
- 62 / 6
The Proton-M, (Протон-М) GRAU index 8K82M or 8K82KM, is an expendable Russian heavy-lift launch vehicle derived from the Soviet-developed Proton. It is built by Khrunichev, and launched from sites 81/24 and 200/39 at the Baikonur Cosmodrome in Kazakhstan. Commercial launches are marketed by International Launch Services (ILS), and generally use Site 200/39. The first Proton-M launch occurred on 7 April 2001.
Propulsion
First stage
6×RD-275M1,746 kN
UDMH / N2O4 · staged-combustion
NPO EnergomashIsp 316s (vac)since 2007
Payloads it launched
60 loaded
LUCH-5X (OLYMP-K 2)
GEO
EXPRESS AMU-3
GEO
EXPRESS AMU-7
GEO
EXPRESS 80
GEO
EXPRESS 103
GEO
MEV-1
GEO
EUTELSAT 5 WEST B
GEO
COSMOS 2539
GEO
YAMAL 601
GEO
COSMOS 2533
GEO
COSMOS 2526
GEO
ASIASAT 9
GEO
AMAZONAS 5
GEO
COSMOS 2520
GEO
ECHOSTAR 21
GEO
INTELSAT 31 (IS-31)
GEO
EXOMARS
Heliocentric
EUTELSAT 9B
GEO
EXPRESS-AMU1
GEO
COSMOS 2513
GEO
TURKSAT 4B
GEO
INMARSAT 5-F3
GEO
EXPRESS-AM7
GEO
INMARSAT 5-F2
GEO
ASTRA 2G
GEO
YAMAL 401
GEO
EUTELSAT 53A
GEO
LUCH (OLYMP-K 1)
GEO
LUCH-5V
GEO
KAZSAT-3
GEO
EXPRESS-AT2
GEO
EXPRESS-AT1
GEO
TURKSAT 4A
GEO
EXPRESS-AM5
GEO
INMARSAT 5-F1
GEO
RADUGA-1M 3
GEO
FM-6
GEO
ASTRA 2E
GEO
SES-6
GEO
EUTELSAT 7B
GEO
ANIK G1
GEO
EUTELSAT 117 WEST A
GEO
NIMIQ 6
GEO
SES-4
GEO
COSMOS 2477 (745)
GLONASS · MEO
COSMOS 2475 (743)
GLONASS · MEO
COSMOS 2476 (744)
GLONASS · MEO
COSMOS 2473
GEO
XM-5
GEO
SES-7 (PROTOSTAR 2)
GEO
ASTRA 1M
GEO
NIMIQ 4
GEO
INMARSAT 4-F3
GEO
AMC-14
GEO
THOR 5
GEO
EXPRESS-AM33
GEO
RADUGA-1M 1
GEO
ASTRA 4A
GEO
ANIK F3
GEO
MEASAT-3
GEO