|
|
Space Shuttle
Engines:
1. 2 × SRM (SRB)
2. 3 × RS-25 (SSME)
2. 2 × AJ10-190 (OME)
|
3. none
1 × Star-48B
1 × Star-63
1 × Orbus-21
1 × Orbus-21H
1 × Orbus-7S
4. none
1 × Orbus-6E |
| PAM-D
| PAM-D2
| IUS
| TOS
| TU-882
| IUS |
Payload mass: |
(LEO) |
24,000
kg |
(204 km, 28.5) |
12,500 kg |
(400
km, 51,6) |
|
(GSTT) |
900 kg
1,110 kg
1,850 kg
6,090 kg
4,944 kg
|
(IRIS)
(PAM-D)
(PAM-D2)
(TOS)
(IUS) |
|
|
(GSO) |
|
2,268 kg |
(IUS) |
|
|
(MoO) |
4,933 kg |
(IUS) |
|
|
(IPT) |
3,550 kg |
(IUS) |
|
|
|
|
|
|
(payload on LEO)
Onyx (Lacrosse), Misty, HST (Hubble), CGRO (Compton), UARS, ERBS
(+solid-fueled upper stage):
(PAM-D) SBS, Anik, Palapa, Westar, Telstar, Morelos, Arabsat, Aussat, ASC, Prowler
(PAM-D2) Satcom-K
(Iris) LAGEOS
(IUS) TDRS, DSCS-3,
DSP, Orion,
AXAF-I (Chandra)
Magellan, Galileo, Ulysses
(Orbus-7S) Quasar,
Leasat (Syncom-4)
(TOS) ACTS
(onboard payload)
Spacelab, Spacehab, Space Radar (SRL), MSL, USMP
(subsidiary free-flyer payload)
MMU, TSS, SPAS, IBSS-SPAS, ORFEUS-SPAS, CRISTA-SPAS, Spartan, Spartan Halley, WSF, PDP
(retrievable payload)
LDEF, Eureca
(ISS) Node (Unity, Harmony, Tranquility), Lab (Destiny), PMA, ITS (S, P, Z), JAM (Quest), COF (Columbus), JLP, JPM (JEM-PM, Kibo), MRM (Ðàññâåò), Cupola, SSRMS (Canadarm), ELC, AMS, STP, MPLM (Leonardo, Rafaello, Donatello)
(Mir) SO (Ñòûêîâî÷íûé îòñåê) |
|
|
|
Additinal operations & services:
|
|
|
retrieved (free-flight payload)
TSS, WSF, Spartan, Spartan Halley, SPAS, IBSS-SPAS, ORFEUS-SPAS, CRISTA-SPAS, PDP, MMU
retrieved (previously launched)
LDEF, Eureca, SFU |
|
retrieved (from ISS)
MPLM
retrieved (after a failure)
Palapa, Westar
service & repair
Hubble, Leasat, SMM, Intelsat
|
|
|
launched by other vehicle (not by Space Shuttle) |
|
|
OV Columbia |
|
OV Challenger |
|
OV Discovery |
|
OV Atlantis |
|
|
OV Endeavour |
|
|
|
Launches: 135 (Failures: 2) /1981-2011/ |
|
|
(Columbia)
(Challenger)
(Discovery)
(Atlantis)
(Endeavour) |
L
28
10
39
33
25 |
F
1
1 |
/1981-2003/
/1983-1986/
/1984-2011/
/1985-2011/
/1992-2011/ |
|
·
·
·
·
·
·
|
PAM-D (11)
PAM-D2
IRIS
IUS
TOS
TU-882 |
21
2
1
15
1
8 |
|
/1982-1990/
/1985-1986/
/1992/
/1983-1999/
/1993/
/1984-1992/ |
|
·
·
·
·
·
· |
Space Radar
Spacelab
Spacehab
USMP
Shuttle-Mir
ISS |
3
22
14
4
9
37 |
|
/1994-2000/
/1983-1995/
/1983-2000/
/1992-1997/
/1995-1998/
/1998-2011/ |
|
|
|
Retired |
|
|
|
Engines:
1. 2 × SRM (SRB)
2. 3 × RS-25 (SSME)
2. 2 × AJ10-190 (OME)
3. 2 × RL-10A-3A | Centaur-T
Payload mass: |
(LEO) |
24,000
kg (204 km, 28.5) |
|
(GSO) |
4,500
kg (G)
6,300 kg (G Prime) |
|
|
Payload: Deep space probes |
|
|
Never flown |
|
|
Space Shuttle-Centaur |
|
|
|
|
|
Retired |
|
|
|
|