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Falcon 9

ACTIVE

First flight: June 4, 2010 · United States · SpaceX

Wikipedia
Falcon 9

Falcon 9 is a two-stage rocket designed and manufactured by SpaceX for the reliable and safe transport of satellites and the Dragon spacecraft into orbit.

KEY SPECIFICATIONS

70m

HEIGHT

3.7m

DIAMETER

549t

MASS

22.8t

PAYLOAD LEO

$50M

PER LAUNCH

2

STAGES

0

BOOSTERS

98%

SUCCESS RATE

68463 kN

TOTAL THRUST

MISSION SUCCESS RATE98%

ENGINE SPECIFICATIONS

TYPE

merlin 1D+

LAYOUT

octaweb

COUNT

9

THRUST/WEIGHT

180.1

THRUST (SL)

845 kN

THRUST (VAC)

914 kN

ISP (SL / VAC)

288s / 312s

ENGINE LOSS MAX

2

liquid oxygen RP-1 kerosene

STAGE DETAILS

S1

First Stage

REUSABLE

Engines9
Fuel385 tons
Burn time162s
Thrust (SL)7607 kN
Thrust (VAC)8227 kN
S2

Second Stage

EXPENDABLE

Engines1
Fuel90 tons
Burn time397s
Thrust934 kN

FAIRING

13.1m × 5.2m

PAYLOAD CAPACITY

Low Earth Orbit
22.8t (50,265 lb)
Geosynchronous Transfer Orbit
8.3t (18,300 lb)
Mars Orbit
4.0t (8,860 lb)

LANDING LEGS

Count: 4Material: carbon fiber

GALLERY

All data sourced from public APIs and publicly available sources. Not affiliated with SpaceX or any other agency.