Russian space rocket adjustment and braking engine to provide center of mass velocity variation during spacecraftorbit correction and spacecraft deceleration
Corrective-braking engine
Technical specifications
Corrective-braking engine (GTD)
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
Reactive control system of automatic spacecraft.
Design features
A four-chamber engine based on four LRE DMT 11D428A-24, integrated into a common fuel component supply system and rigidly mounted on a bracket.
The level of development
The letter "O". Flight operation
Russian space rocket adjustment and braking engine to provide center of mass velocity variation during spacecraftorbit correction and spacecraft deceleration