This mission is both a return to flight for SpaceX after the upper stage failure earlier this summer and the first flight of a major upgrade to Falcon 9 named Falcon 9 Full Thrust.
The Falcon 9 FT performance numbers have been increased 33% over the previous version, and will also be used as Falcon Heavy side booster cores. A second, further upgraded, version will be used as the Falcon Havy center core. Falcon Heavy's first flight has been delayed to April-May 2016 because of the F9 upper stage failure investigation.
The upper stage failure was caused by a defective strut holding down a helium tank which failed at just 20% of it's rated load. The supplier has been replaced.
The Falcon 9 Full Thrust test fire for the SES-9 comment launch will be done on the new Falcon 9/Falcon Heavy test stand at McGregor TX.
Falcon 9 Full Thrust upgrades
Height increased from 68.28 m (224 ft) to 70m (229.6 ft)
Stage 2 lengthened
M1DVac Stags 2 engine thrust increased;
Vac thrust: 934 kN (210,000 lbf)
M1DVac nozzle lengthened
Interstage lengthened & strengthened
New center pusher to guide Stage 2 separation
Grid fin design evolved (for stage landings)
Stage 1 structural upgrades
Landing legs upgraded
Octaweb thrust structure upgraded
Merlin 1D thrust upgraded;
SL thrust: 6,806 kN (1,530,000 lbf)
Vac thrust: 7,426 kN (1,669,500 lbf)
Propellants supercooled to increase bulk density
Dragon 2 shown (commercial & NASA crew spacecraft)
falcon9-render.jpg
The Falcon 9 FT performance numbers have been increased 33% over the previous version, and will also be used as Falcon Heavy side booster cores. A second, further upgraded, version will be used as the Falcon Havy center core. Falcon Heavy's first flight has been delayed to April-May 2016 because of the F9 upper stage failure investigation.
The upper stage failure was caused by a defective strut holding down a helium tank which failed at just 20% of it's rated load. The supplier has been replaced.
The Falcon 9 Full Thrust test fire for the SES-9 comment launch will be done on the new Falcon 9/Falcon Heavy test stand at McGregor TX.
Peter B. de Selding â€@pbdes* 2m2 minutes ago
SES: No earlier than Nov 17 for SpaceX Falcon 9 v1 upgrade flight of SES-9. 15-second ignition of denser-fueled 1st stage this week.
SES: No earlier than Nov 17 for SpaceX Falcon 9 v1 upgrade flight of SES-9. 15-second ignition of denser-fueled 1st stage this week.
Height increased from 68.28 m (224 ft) to 70m (229.6 ft)
Stage 2 lengthened
M1DVac Stags 2 engine thrust increased;
Vac thrust: 934 kN (210,000 lbf)
M1DVac nozzle lengthened
Interstage lengthened & strengthened
New center pusher to guide Stage 2 separation
Grid fin design evolved (for stage landings)
Stage 1 structural upgrades
Landing legs upgraded
Octaweb thrust structure upgraded
Merlin 1D thrust upgraded;
SL thrust: 6,806 kN (1,530,000 lbf)
Vac thrust: 7,426 kN (1,669,500 lbf)
Propellants supercooled to increase bulk density
Dragon 2 shown (commercial & NASA crew spacecraft)
falcon9-render.jpg
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