HARDWARE / PRODUCT

Cyclone-4M

Yuzhnoye Design Bureau (KB Pivdenne)
Cyclone-4M

Two-stage light-lift launch vehicle in development by Yuzhnoye in partnership with Canada's Maritime Launch Services.

Technical specifications

Height
38.7 m
Diameter
4.0 m
First stage mass
260,700 kg
Second stage mass
14,000 kg
Payload to 200 km LEO
5,000 kg
Payload to GTO
910 kg
Stages
2
Status
In development

About

Cyclone-4M is a modern two-stage light-lift launch vehicle developed by Yuzhnoye Design Bureau as the successor to the earlier Tsyklon (Cyclone) rocket family. The vehicle’s commercial development is managed in partnership with Maritime Launch Services, a Canadian company that originally planned to operate Cyclone-4M from Spaceport Nova Scotia near Canso, Nova Scotia. The first stage is powered by four RD-870 engines burning kerosene and liquid oxygen, generating roughly 3,130 kN of thrust at sea level, while the second stage uses a single storable-propellant RD-861K engine. Cyclone-4M is designed to deliver payloads of up to 5,000 kg to a 200 km low Earth orbit or approximately 910 kg to geostationary transfer orbit. Second-stage qualification testing was completed in October 2019, but the program has faced significant schedule uncertainty following Russia’s full-scale invasion of Ukraine in 2022, and Maritime Launch Services terminated its agreement to launch Cyclone-4M from Spaceport Nova Scotia by the third quarter of 2024, leaving the vehicle’s launch site and timeline under review.

Documentation

No public datasheet yet — request the datasheet / ICD from the supplier.

Source: en.wikipedia.org ↗