|
|purpose= Ana aşama motoru, [[Yukarı aşama]] motoru
|associated= [[Falcon 9]], [[Falcon Heavy]]
|type=sıvı
|fuel=[[RP-1]] (roket-sınıfı kerosen)
|oxidiser=[[LOX]]
|capacity=
|thrust(Vac)=801 [[Newton (birim)|kN]]<ref name=sxf9ProductPage20130808>
{{cite web
| title = SpaceX Falcon 9 product page
| url = http://www.spacex.com/falcon9
| accessdate = 2015-05-04
}}
</ref>
|thrust(SL)=654 kN<ref name=sxf9ProductPage20130808>
{{cite web
| title = SpaceX Falcon 9 product page
| url = http://www.spacex.com/falcon9
| accessdate = 2015-05-04
}}
</ref>
|specific_impulse_vacuum= 340 s (3.34 km/s)<ref name=sxf9ProductPage20130808>
{{cite web
| title = SpaceX Falcon 9 product page
| url = http://www.spacex.com/falcon9
| accessdate = 2015-05-01
}}
</ref>
|specific_impulse_sea_level= 282 s (2.73 km/s)<ref name=spacexfalcon9page/>
|chamber_pressure={{convert|1410|psi|MPa|abbr=on|disp=flip|lk=in}}<ref name=awst20110811/>
|thrust_to_weight=150<ref name=a&s201201/>
|cycle=[[Gas-generator cycle (rocket)|gas-generator]]
<!-- todo: add dimensions (diameter, length, dry_weight) -->
|diameter=
|height={{convert|00|mm|abbr=on|disp=flip|sp=us}}
|Weight, dry={{convert|00|kg|abbr=on}}
}}
| 