NASASpaceFlight.com Forum
General Discussion => Q&A Section => Topic started by: JoeFromRIUSA on 05/22/2023 10:13 pm
-
UDHM/N204 or Lox/RP-1
-
The first reasonable looking source I found (https://www.researchgate.net/figure/Characteristic-data-of-typical-liquid-propellants_tbl1_225022069) gives the following:
LOX/RP-1: 358s
N2O4/UDMH: 342s
Of course these will vary with O/F ratio, pressure, and other factors but this ought to be a decent comparison.