MRM-106

MRM-106B
Credit - Aerojet Redmond
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Designer: Aerojet Redmond. Propellants: Hydrazine. Thrust(vac): 27 N (6 lbf). Isp: 231 sec. Burn time: 2,991 sec. Mass Engine: 0.94 kg (2.07 lb). Diameter: 0.0310 m (0.1010 ft). Length: 0.17 m (0.56 ft). Chambers: 1. Country: USA. Status: In Production.

Steady-state thrust 9 N.  
 
 
 
 
 
 
 
 


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