N.A.S.A. | Space Shuttle SSME Block-I |
Space Shuttle SSME Block-IA |
Space Shuttle SSME Block-IIA |
Space Shuttle SSME Block-II |
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Overall Vehicle |
Operational | from | 20.10.1995 | 12.01.1997 | 23.01.1998 | 08.04.2002 | ||||
to | 20.06.1996 | 02.06.1998 | 01.03.2002 | 08.07.2011 | ||||||
Orbital flights | 4 | 5 | 17 | 27 | ||||||
Payload weight | t | STS-78 | 10.675 | STS-82 | 7.588 | STS-101 | 14.622 | STS-113 | 14.934 | |
Gross liftoff weight | t | ~2,049 |
2,047.27 |
2,050.11 |
2,050.78 | |||||
Gross propellant weight | t | < 1,749.32 | < 1,749.32 | < 1,751.18 | < 1,751.18 | |||||
Total length | m | 56.14 | 56.14 | 56.14 | 56.14 | |||||
Max. diameter (span) | m | 23.79 | 23.79 | 23.79 | 23.79 | |||||
Total liftoff thrust (s.l.) | kN | 31,827 | 31,8278 | 31,827 | 31,827 | |||||
Total impulse (vac) | MN*s | < 5,938.6 | < 5,938.6 | < 5,927.0 | < 5,927.0 | |||||
Bay |
Total length | m | 18.29 | 18.29 | 18.29 | 18.29 | ||||
Diameter | m | 4.57 | 4.57 | 4.57 | 4.57 | |||||
Total weight | t | - | - | - | - | |||||
Orbiter |
Name | Columbia | Discovery | Atlantis | Endeavour | |||||
Length | m | 37.24 | 37.24 | 37.24 | 37.24 | |||||
Diameter | m | |||||||||
Liftoff weight (excl. payload) | t | 105.523 | ? | ? | 101.526 | |||||
Propellant weight | t | < 21.65 | < 21.65 | < 21.65 | < 21.65 | |||||
Engines | 2 OMS | AJ-10-190 | AJ-10-190 | AJ-10-190 | AJ-10-190 | |||||
Propellant |
MMH/N2O4 |
MMH/N2O4 |
MMH/N2O4 |
MMH/N2O4 |
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Total thrust (vac) | kN | 53.38 | 53.38 | 53.38 | 53.38 | |||||
Specific impulse (vac) | N*s/kg | 2886 | 2886 | 2886 | 2886 | |||||
Burn time | s | < 1,170 | < 1,170 | < 1,170 | < 1,170 | |||||
Total impulse (vac) | MN*s | < 62.5 | < 62.5 | < 62.5 | < 62.5 | |||||
Stage 1 |
Name | LWET | LWET | SLWET | SLWET | |||||
Length | m | 46.88 | 46.88 | 46.88 | 46.88 | |||||
Diameter | m | 8.41 | 8.41 | 8.41 | 8.41 | |||||
Liftoff weight | t | 754.58 | 754.58 | 753.03 | 753.03 | |||||
Propellant weight | t | 724.25 | 724.25 | 726.11 | 726.11 | |||||
Engines | 3 | Rock. SSME-I | Rock. SSME-IA | Rock. SSME-IIA | Rock. SSME-II | |||||
Propellant | LH2/LOX | LH2/LOX | LH2/LOX | LH2/LOX | ||||||
Total thrust (s.l.) | kN | 5,004.0 | 5,004.0 | 5,004.0 | 5,004.0 | |||||
Specific impulse (s.l.) | N*s/kg | 3564 | 3564 | 3541 | 3541 | |||||
Burn time | s | 511 | 511 | 507.5 | 507.5 | |||||
Total impulse (vac) | MN*s | 3,233.8 | 3,233.8 | 3,222.2 | 3,222.2 | |||||
Booster |
Name | 2 RSRM | 2 RSRM | 2 RSRM | 2 RSRM | |||||
Length | m | 45.46 | 45.46 | 45.46 | 45.46 | |||||
Diameter | m | 3.71 | 3.71 | 3.71 | 3.71 | |||||
Liftoff weight | t | 1,178.20 | 1,178.20 | 1,178.20 | 1,178.20 | |||||
Propellant weight | t | 1,003.42 | 1,003.42 | 1,003.42 | 1,003.42 | |||||
Engines | Thiokol | Thiokol | Thiokol | Thiokol | ||||||
Propellant | solid PBAN | solid PBAN | solid PBAN | solid PBAN | ||||||
Total thrust (s.l.) | kN | 26,823 (max) | 26,823 (max) | 26,823 (max) | 26,823 (max) | |||||
Specific impulse (s.l.) | N*s/kg | 2383 | 2383 | 2383 | 2383 | |||||
Burn time | s | 122.2 | 122.2 | 122.2 | 122.2 | |||||
Total impulse (vac) | MN*s | 2,642.3 | 2,642.3 | 2,642.3 | 2,642.3 |