There are 17 images added between 21 June 2009 and 23 December 2014
1  2  3  
Angara A5  
Initial Operational Capability (IOC): 2016
Maiden Flight: 23 December 2014
Total Production: 1
Origin: Russia
Corporations: Khrunichev Space Center
Parent System: Angara LS
Initial Operational Capability (IOC): 2015
Maiden Flight: 9 July 2014
Total Production: 2
Family Members: Angara 1.1, Angara 1.2PP, Angara A3, Angara A5V and Angara A7
Reviews
There are no reviews so far

Description: The Angara is a family of space launch vehicles being built on the basis of a Common Core Booster (CCB) or Common Rocket Module (CRM) using the RD-191 reusable liquid fuel engine. The program was launched in 1995 and its main purpose is to ensure space access for the Russian Ministry of Defense for several decades from Plesetsk launch site. The Angara family comprises small-, medium- and heavy-lift space vehicles which can be launched from the same pad in Plesetsk. Its key component of the CCB/CRM is the environment-friendly liquid oxygen (LOX) kerosene RD-191 engine. The Angara family can put payloads into low-Earth orbit weighing from 2,000 to 24,500 kg, or up to 4,500 kg into geosynchronous orbit. The first Angara space launch system is expected to lift-off after 2010.

The Angara A5 is a two-stage, heavy-lift space launch vehicle comprising five Common Core Boosters (CCBs) at the first stage, including four Baikal reusable boosters; one 66,200-lb RD-0124 motor at the second stage; and the Breeze M or KVRB upper stage. With a maximum lift-off weight of 773-ton the Angara A5 can put into low-Earth orbit payloads of up to 24,500 kg. Besides, the Breeze M or KVRB can lift payloads of up to 7,300 kg (or 5,400 kg) to a geo-transfer orbit at 5,500 km of altitude and 25-degree of inclination or place directly payloads of up to 4,500 kg (or 2,900 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. The Breeze M is also available in a larger version with 5.1 meters diameter and16.37 meters in length. The KVRB has a diameter of 5.1 meters and 19.65 meters in length.

Angara A5 Specifications

Crew: 0
Number of Stages: 3
Dimensions
Height: 55 meter (2,169 inch)
Rocket Diameter: 4.35 meter
Performance
Orbit: 36,000 kilometer (22,374 mile)
Weight
Max Lift-off Thrust: 1,060 ton (2,336,861 pound)
Max Lift-off Weight: 773 ton (1,704,145 pound)
Payload to GEO: 4,500 kilogram (9,921 pound)
Payload to GTO: 7,300 kilogram (16,093 pound)
Payload to LEO: 24,500 kilogram (54,012 pound)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Angara A5 News

There are 4 news between
23 Dec 2014 and 2 Apr 2016
Saturday, April 2, 2016Angara A5V Rocket to Be Ready for Lunar Missions by 2025
Wednesday, July 15, 2015Launch of the First Manned Angara Rocket is Planned for 2023
Wednesday, April 22, 2015Russia to Develop Angara A5B Super-Heavy Carrier Rocket
Tuesday, December 23, 2014Russia Successfully Completes First Launch of Angara A5 Heavy Space Rocket

Operators & Related Equipment


OperatorsItems

Grand Total 11
Propulsion Systems
Baikalx4
RD-191x1
Copyright © 2003-2017 deagel.com website. All rights reserved.
This website has been optimized for HTML 5 and CSS 3.