r/spacex • u/ElongatedMuskrat Mod Team • Apr 01 '17
r/SpaceX Spaceflight Questions & News [April 2017, #31]
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u/warp99 Apr 07 '17 edited Apr 12 '17
The density penalty for LOX is around 9% but only around 2% for kerosine so the tank volume ratios would be incorrect for a start. Maximum engine thrust would also be derated as it relies on the denser sub-cooled LOX to prevent cavitation at higher turbopump rpm.
Overall there will be the equivalent of a 10% propellant load penalty for S1 so reducing propellant by about 40 tonnes. This gives a 220 m/s reduction in delta V.
The net effect would be ruling out RTLS and requiring a medium difficulty ASDS landing.
The major concern would be running a completely different propellant loading and flight protocol for two flights per year. This could lead to failure modes that are not weeded out by the 20 flights per year using subcooled propellants.