MR-107U 300N

Name: MR-107U 300N
Brand: Aerojet Rocketdyne

Vendor profile

Overview

MR-107U 300N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 1.38 kg (includes engine and valves), with a specific impulse of 223 to 229 sec and a thrust of 182 to 307 N (steady state).

Looking for more information or want to purchase?

Contact now

Overview

Name: MR-107U 300N
Vendor: Aerojet Rocketdyne
Subsystem: Propulsion Subsystem
Component Type: Monopropellant Thruster
Form Factor: SmallSat
Heritage: Yes

Vendor Details

Name: Aerojet Rocketdyne
Website: https://www.rocket.com/
Founded: 1942

Vendor Request for Information Form

Name (required)

Email (required)

Country (required)

Phone (optional)

Message (required) Max. 1000 characters

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

Specifications

Subsystem: Propulsion Subsystem
Component Type: Monopropellant Thruster
Form Factor: SmallSat
Vendor: Aerojet Rocketdyne
Dry Mass: 1.38 kg
Average Power: 52.0 W
Heritage: Yes
Status: In Production

Datasheet

Try Designer

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

Launch designer

Aerojet Rocketdyne

View all products

Similar Components

MR-104H 510N

Aerojet Rocketdyne

MT-6

IHI Aerospace

CZ-11-600

SITAEL

MR-80B 3100N

Aerojet Rocketdyne