NEXT SPACEFLIGHT
NEXT SPACEFLIGHT

Angara 1

The Angara 1 variants use a single Universal Rocket Module (URM-1) core as the first stage. The URM-1 is powered by a single NPO Energomash RD-191 engine burning liquid oxygen and RG-1 (Soviet kerosene).

Missions: 3
Successes: 3
Partial Failures: 0
Failures: 0
Success Streak: 3
Success Rate: 100%
Wiki

Configurations

Angara 1.2
Image Credit: VKS RF
Khrunichev
Status: Active
Liftoff Thrust: 1,922 kN
Payload to LEO: 3,800 kg
Payload to GTO: 0 kg
Stages: 2
Strap-ons: 0
Rocket Height: 42.7 m
Fairing Diameter: 3.0 m
Fairing Height: 2.9 m
Wiki
Angara 1.2PP
Image Credit: VKS RF
Khrunichev
Status: Retired
Liftoff Thrust: 1,922 kN
Payload to GTO: 0 kg
Stages: 2
Strap-ons: 0
Rocket Height: 42.7 m
Fairing Diameter: 3.0 m
Fairing Height: 2.9 m
Wiki

Launch Sites

Site 35/1, Plesetsk Cosmodrome, Russia
Site 1A, Vostochny Cosmodrome, Russia

Launches

VKS RF
Angara 1.2 | Cosmos 2560
Sat Oct 15, 2022 19:55 UTC
Site 35/1, Plesetsk Cosmodrome, Russia
VKS RF
Angara 1.2 | Cosmos 2555
Fri Apr 29, 2022 19:55 UTC
Site 35/1, Plesetsk Cosmodrome, Russia
VKS RF
Angara 1.2PP | Demo Flight
Suborbital
Wed Jul 09, 2014 12:00 UTC
Site 35/1, Plesetsk Cosmodrome, Russia