Aerojet 445
Designer: Aerojet. Propellants: N2O4/MMH. Thrust(vac): 445 N (100 lbf). Isp: 309 sec. Mass Engine: 1.86 kg (4.10 lb). Chambers: 1. Area Ratio: 150.00. Thrust to Weight Ratio: 24.39. Country: USA. Status: In Production.

Mixture Ratio(O/F): 1.65.  
 
 
 
 
 
 
 
 

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