TH-31
TH-31 are conventional propellant liquid rocket engines with
multiple starts and storability used in upper stage propulsion systems
Propellant
NTO/MMH
Configuration
1x3000N+8x150 N
Specific impulse,vacuum
306s
Total impulse
2.16MN.S
Reusability
150N ≥2000Times3000N≥20Times
weight,dry
≯160Kg
weight,wet
940Kg
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