Re: Upcoming SpaceX Falcon 9 Flight 1 Launch
I've been trying to pin down data for the Block 1 Falcon 9 that will make this flight attempt. SpaceX has provided some information for the projected Block 2 Falcon 9 in its User Guide, but numbers are harder to come by for the Block 1.
Here is what we know about Block 1, based upon information on the SpaceX update pages.
Stage 1:
Thrust (sea level) = 401.43 tonnes
Burn Time = 178 seconds
Propellant Burn Rate = 1.4595 tonnes per second
Total Propellant Burned = 259.8 tonnes
Specific Impulse = 275/304 sec (SL/vac)
Dry mass > 15.4 tonnes
Stage 2:
Thrust (vacuum) = 41.96 tonnes
Burn Time = 329 seconds
Specific Impulse = ~342 sec (vac)
If the Stage 2 Vacuum Merlin ran at full throttle during its burn, it would consume 40.4 tonnes of propellant. SpaceX has not revealed the throttle profile, however, so I don't know the propellant mass for certain.
Payload:
A couple of years ago, SpaceX claimed 9.9 tonnes payload to LEO for Block 1, presumably to a 28.5 deg inclination. Dragon only weighs 8 tonnes fully loaded, but that is to a 51.6 degree inclination. It should be possible for Falcon 9 Block 1 to orbit 8 tonnes with usable stage propellant mass ratios in the 0.93 to 0.94 range. That implies a gross liftoff mass of approximately 320 tonnes (not including payload), which is about 13.4 tonnes less than the Block 2 Falcon 9 number given in the User Guide. That gives a respectable 1.25 liftoff thrust to weight ratio.
- Ed Kyle