Yuzhnoye's new liquid rocket engines as enablers for space exploration
Autor: | Alexander Kushnaryov, Alexander Degtyarev, Vladimir Shulga, Oleg Ventskovsky |
---|---|
Rok vydání: | 2016 |
Předmět: |
Propellant
020301 aerospace & aeronautics Engineering business.product_category business.industry Liquid-propellant rocket Rocket engine nozzle Aerospace Engineering Thrust 02 engineering and technology Propulsion Automotive engineering 020303 mechanical engineering & transports 0203 mechanical engineering Rocket Specific impulse Aerospace engineering Liquid oxygen business |
Zdroj: | Acta Astronautica. 127:693-698 |
ISSN: | 0094-5765 |
Popis: | Advanced liquid rocket engines (LREs) are being created by Yuzhnoye Design Office of Ukraine based on the fifty-year experience of rocket engines' and propulsion systems' development. These LREs use both hypergolic (NTO+UDMH) and cryogenic (liquid oxygen+kerosene) propellants. First stage engines have a range of thrust from 40 to 250 t, while the upper stage (used in space) engines - from several kilograms to 50 t and a re-ignition feature. The engines are intended for both Ukraine”s independent access to space and international market. |
Databáze: | OpenAIRE |
Externí odkaz: |