Initial Operational Capability (IOC): 2010
Total Production: ?
Origin: Ukraine
Corporations: National Space Agency of Ukraine (operation), Yuzhmash (production) and Yuzhnoye (design)
Parent System: Mayak
Initial Operational Capability (IOC): 2010
Total Production: ?
Family Members: Mayak-12 and Mayak-22
There are no reviews so far

Description: The Mayak is a family of space launch system being developed by National Space Center of Ukraine, Yushnoye design bureau and Yushmash machine-building plant for the global launch services market. The projected family members are based on a modular design with tandem rockets and multiple stages with the option to add strapon rocket boosters enabling greater payloads. Employing a mixture of oxygen and kerosene liquid fuel, these vehicles will lift-off with a mass ranging from 130 to 320 tons. The Mayak space launch vehicle family leverages existing and under development space technologies and is influenced by current Zenit and Cyclone rockets.

The Mayak-23 is the larger member of the Mayak family having three stages and a maximum lift-off mass of 320t. It has the same diameter than Mayak-22 rocket but has a longer fuselage homing a third stage.

Mayak-23 Specifications

Number of Stages: 3
Height: 46,375 millimeter (1,826 inch)
Rocket Diameter: 3.90 meter
Max Lift-off Weight: 320 ton (705,467 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)

Operators & Related Equipment


Grand Total ?1
Copyright © 2003-2019 website. All rights reserved.
This website has been optimized for HTML 5 and CSS 3.