Proton / UR-500 family
UR-500
Proton is an expendable launch system used for both commercial and Russian government space launches. The first Proton rocket was launched in 1965.
Flights flown4
Success rate75%3/4
Payload to LEO8,400kg
Maiden flight1965-07-16
Peak year19652 flights
UR-500 is built by Khrunichev State Research and Production Space Center of Russia. It first flew on 16 July 1965 and last flew on 6 July 1966.
Flight record
75% success rate3 of 4 flown · 1 failed
1965peak 1965 · 2 flights1966
First flight1965-07-16
Latest flight1966-07-06
Failures1
Consecutive successes1
Fastest turnaround103d 22h
Payload
| Low Earth orbit | 8,400kg |
|---|
Vehicle
| Stages | 2 |
|---|---|
| Length | 46.28m |
| Diameter | 4.15m |
| Launch mass | 595t |
| Liftoff thrust | 8,847kN |
| Maiden flight | 1965-07-16 |
| Reusable | No |
Pads used
Orbits delivered
Low Earth Orbit4
Launch history
| Date | Mission | Pad | Orbit | Outcome |
|---|---|---|---|---|
| 1966-07-06 | UR-500 | Proton 3 | 81/23 (81L) | Low Earth Orbit | Success |
| 1966-03-24 | UR-500 | Proton 3a | 81/23 (81L) | Low Earth Orbit | Failure |
| 1965-11-02 | UR-500 | Proton 2 | 81/23 (81L) | Low Earth Orbit | Success |
| 1965-07-16 | UR-500 | Proton 1 | 81/23 (81L) | Low Earth Orbit | Success |
Specifications from Launch Library 2 by The Space Devs, launch records from Space Index. Derived figures are computed here; see sources and method.
Further reading: Wikipedia