Is a
Product attributes
Industry
Other attributes
Date Invented
2001
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
The Almaz and Mir orbital stations (Kvant, Kristall, Spectrum, and Nature modules), the Zarya module of the International Space Station, and the Briz upper stage.
The level of development
The letter "O". Flight operation
Timeline
No Timeline data yet.
