200N Biprop Thruster

200N Biprop Thruster image

Overview

The 200N bipropellant engine was developed and qualified for application as attitude control, maneuvering and braking thruster of ESA‘s ATV.


The engine is designed to be capable of both steady-state and pulse mode in a very broad regimes of inlet conditions and exhibits outstanding thermal and combustion stability even at extreme conditions. To meet the specific FDIR needs of man rated missions, the engine is equipped with several flight temperature sensors for e.g. in-flight leak detection and a combustion pressure transducer.

Looking for more information or want to purchase?

Overview

Name
200N Biprop Thruster
Form Factor
SmallSat
Heritage
Yes

Vendor Details

Name
ArianeGroup
Founded
2015

Vendor Request for Information Form

Max. 1000 characters

Please include a detailed description in your message. This helps vendors to better understand your request.

Specifications

Form Factor
SmallSat
Dry Mass
1.9 kg
Average Power
N/A
Heritage
Yes
Status
In Production
  • Designer logo

    Try Designer

    Design, model, and evaluate satellite mission concepts quickly with our software.

  • ArianeGroup

    View all products