Angara A3
Angara A3
Space Launch Systems
Basic Information
Name
Angara A3
Designation
Angara A3
Alternate Designation
—
Equipment Type
Space Launch Systems
Manufacturer
Khrunichev Space Center
Date of Introduction
2016
Description
The Angara A3 is a two-stage, medium-lift space launch vehicle comprising three Common Core Boosters (CCBs) at the first stage, including two Baikal reusable boosters; one 62,000-lb RD-0124 motor at the second stage; and the Breeze M upper stage. With a maximum lift-off weight of 480-ton the Angara A3 can put into low-Earth Orbits payloads of up to 14,000 kg. Besides, the Breeze M can lift payloads of up to 3,700 kg (or 2,400 kg) to a geo-transfer orbit at 5,500 km of altitude and 25-degree of inclination or place directly payloads of up to 2,000 kg (or 1,000 kg) into geostationary orbit. The Breeze M upper stage has a diameter of 4.35 meters and 11.6 or 15.25 meters in length.
Overview (Deagel)
Group
Space Launch Systems
Status
Cancelled
Origin
Russia
Contractor
Khrunichev Space Center
Initial Operational Capability (IOC)
2016
Total Production
?
Specifications (Deagel)
Crew
0
Number of Stages
3
Dimensions — Height
46.7 meter
Dimensions — Rocket Diameter
4.4 meter
Mass — Max Lift-off Thrust
636 ton
Mass — Max Lift-off Weight
480 ton
Mass — Payload to GEO
2,000 kilogram
Mass — Payload to GTO
3,700 kilogram
Mass — Payload to LEO
14,000 kilogram
Performance — Orbit
36,000 kilometer
Gear (Deagel)
Item 1
Rocket Engines: Baikal (2)
Item 2
Rocket Engines: RD-191 (1)
Variants
Variant 1
Angara 1.1
Variant 2
Angara A3
Variant 3
Angara A7
Variant 4
Angara 1.2
Variant 5
Angara A5
Variant 6
Angara A5M
Variant 7
Angara A5V
Details
Country of Origin
Russia
Sources
deagel.com: https://www.deagel.com/x/x/a000232
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
—
Width
4.4 m
Height
46.7 m
Weight
480000 kg
Operators (1)
Russia
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