Is a
Product attributes
Launch Date
2015
Founder
Technical specifications
Two-component low-thrust rocket engine
Fuel: NDMG/ATIN
Function
Creation of a multiple force pulse in the process of orientation and stabilization of the spacecraft by commands received from the quality management system.
Application
By the beginning of 2015, 1,385 engines of this type were operated as part of the Almaz orbital station, the Briz upper stage, the retrofitting modules of the Mir orbital station – Kvant-2, Kristall, Spectrum, Nature, the first Russian Zarya module of the International Space Station and the upper stage of the Strela launch vehicle.
The level of development
The letter "O". Flight operation
Timeline
No Timeline data yet.
Further Resources
No Further Resources data yet.