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Titan 2 |
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Titan 2 (SM-68B)
Engines:
1. 2 × LR-87-5
2. 1 × LR-91-5
Total mass: 154,000 kg
Maximum range: 11,690 km
Warhead: 3,100 kg
Fairing:
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Launches: 81 (Failures: 15) /1962-1976/
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Titan 2 GLV |
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Titan 2 GLV Engines:
1. 2 × LR-87-5
2. 1 × LR-91-5
Total mass: 150,530
kg
Payload (LEO): 3,600 kg
Fairing: (G) - Gemini
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Launches: 12 (Failures: 0) /1964-1966/
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Star-13E × 4 (retro motor) |
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Retired |
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Titan 2 (23) G |
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Titan 2 (23) G
Engines: |
1. |
2 × |
LR-87-5 |
2. |
1 × |
LR-91-5 |
|
3. |
1 ×
1 × |
none Star-37S | ISS
Star-37XFP | ISS |
Total mass: 150,530
kg
Payload:
(LEO)
(LPEO) |
3,600 kg
2,177 kg
|
Fairing:
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Launches: 13 (Failures: 1) /1988-2003/
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L |
F |
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·
· 37FM
· 37S
· 37XFP |
5
1
1
6 |
1 |
/1988-2003/
/1994/
/1997/
/1993-2003/ |
Payload:
(–) Farrah (USA), Coriolis, QuikSCAT
( 37FM) Clementine
( 37S) DMSP
( 37XPF) DMSP, Landsat, NOAA |
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Star-37FM (DSPSE-ISA) |
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R-4D |
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Retired |
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Titan 3A |
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Titan 3A Engines:
1. 2 × LR-87-9
2. 1 × LR-91-9
3. 2 × AJ10-138 | Transtage
Total mass: 161,730 kg
Apogee: 4,000 km
Payload (LEO): 3,175 kg
Fairing:
(1) |
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Launches: 4 (Failures: 1) /1964-1965/
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Star-13A |
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Retired |
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Titan 3B |
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Titan 3B Engines:
1. 2 × LR-87-9
2. 1 × LR-91-9
3. 1 × Bell 8096 | Agena D
Total mass: 156,540 kg
Apogee: 185 km
Payload (LEO): 3,300 kg
Fairing:
(2) |
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Launches: 22 (Failures: 1) /1966-1970/
Payload: KH-8
(Gambit-3 Block 1) |
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Star-12 (retro motor) |
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Retired |
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Titan 3 (23) B |
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Titan 3 (24) B |
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Titan 3 (33) B |
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Titan 3 (34) B |
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Titan 3 (23) B Engines:
1. 2 × LR-87-11
2. 1 × LR-91-11
3. 1 × Bell 8096 | Agena D
Total mass: 165,000 kg
Apogee: 1,000 km
Payload (LEO): 3,300 kg |
Payload:
(LEO)
(LPEO) |
~ 3,500 kg
~ 700 kg |
Fairing:
|
(3)
(31)
(32) |
- KH-8 (Gambit-3)
- Quasar
- Jumpseat |
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Launches: 46 (Failures: 3) /1969-1987/
(3 (23) B)
(3 (24) B)
(3 (33) B)
(3 (34) B) |
L
9
23
3
11 |
F
2
1 |
/1969-1971/
/1971-1984/
/1971-1973/
/1975-1987/ |
Payload:
(3 (23) B) KH-8
(Gambit-3 Block 2)
(3 (24) B) KH-8
(Gambit-3 Block 2 / 3 / 4)
(3 (33) B) Jumpseat
(3 (34) B) Jumpseat, Quasar |
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Star-12 (retro motor) |
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Retired |
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Total mass: 626,190 kg
Payload:
(LEO)
(GSTT)
(GSO) |
13,100 kg
3,000 kg
1,400 kg |
Fairing:
|
(1)
(G)
(21)
(22)
(23)
(24) |
- LCS, LES, IDCSP
- Gemini-B / MOL
- Vela
- TACSAT, ATS
- DSCS-2, DSP
- Chalet (Vortex) |
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Launches: 36 (Failures: 6) /1965-1982/
(3C)
(3 (23) C) |
L
14
22 |
F
3
3 |
/1965-1970/
/1970-1982/ |
Payload:
(3C) LCS, LES, OV2, OSCAR, IDCSP, Vela, TACSAT,
(Gemini-B, OV1, OV3, OV4),
(3 (23) C) DSCS-2, DSP, Chalet (Vortex), ATS, (LES, Solrad) |
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BE-3A / B
Star-17A |
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ion engines |
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Retired |
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Titan 3C |
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Titan 3 (23) C |
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Titan 3 (23) D |
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Titan 3 (23) D Engines:
0. 2 × UA1205
1. 2 × LR-87-11
2. 1 × LR-91-11
Total mass: 612,990 kg
Apogee: 1,000 km
Payload:
(LEO)
(LPEO) |
12,300 kg
10,900 kg |
Fairing:
|
(33)
(34) |
- KH-9 (Hexagon)
- KH-11 (Kennen) |
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Launches: 22 (Failures:
0) /1971-1982/
Payload: KH-9 (Hexagon),
KH-11 (Kennen / Crystal) |
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Bell 8096 | Agena D
( ? ) |
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Star-12 (retro motor) |
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Retired |
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Titan 3 (34) D |
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Titan 3C IUS |
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Titan 3C Transtage |
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Titan 3 (34) D
Engines: |
0. |
2 × |
UA1206 |
1. |
2 × |
LR-87-11 |
2. |
1 × |
LR-91-11 |
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3. |
2 ×
1 × |
none
AJ10-138 | Transtage
Orbus-21 | IUS |
|
3. |
1 × |
none Orbus-6E | IUS |
Total mass: |
723,490 kg
720,000 kg
725,000 kg |
(34D)
(34D Transtage)
(34D IUS) |
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Apogee: |
185 km
40,000 km
40,000 km |
(34D)
(34D Transtage)
(34D IUS) |
|
Payload:
(LEO)
(LPEO)
(GSTT) |
14,515 kg
13,600 kg
5,000 kg |
Fairing:
|
(33)
(34)
(23)
(24)
(25) |
- KH-9 (Hexagon)
- KH-11 (Kennen)
- DSP
- Vortex, Mercury
- DSCS-2 / 3 |
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Launches: 15 (Failures: 3) /1982-1989/
(34D)
· IUS
· Transtage |
L
7
1
7 |
F
2
1 |
/1983-1988/
/1982-1982/
/1984-1989/ |
Payload:
(34D) KH-9 (Hexagon), KH-11 (Kennen / Crystal)
(34D Transtage) DSP, Vortex, Mercury, DSCS-2 (D)SCS-3
(34D IUS) DSCS-2 (D)SCS-3 |
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Bell 8096 | Agena D
( ? ) |
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Star-12 (retro motor) |
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Retired |
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Titan 3 (23) E |
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Titan 3 (23) E Engines:
0. 2 × UA1205
1. 2 × LR-87-11
2. 1 × LR-91-11
3. 2 × RL-10A-3 | Centaur
Total mass: 632,970 kg
Apogee: 400,000 km
Payload:
(LEO)
(GSTT)
(GSO)
(IPT) |
17,000 kg
6,800 kg
3,200 kg
5,000 kg |
Fairing:
(41) |
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Launches: 7 (Failures: 1) /1974-1977/
Payload: Sphinx, Viking,
Helios, Voyager |
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Retired |
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Commercial
Titan 3 |
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Commercial Titan 3 (34)
Engines: |
0. |
2 × |
UA1206 |
1. |
2 × |
LR-87-11 |
2. |
1 × |
LR-91-11 |
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3. |
|
none 3.
Orbus-21S Orbus-21H | TOS-21H Star-63 | PAM-D2 |
|
3. |
1 × |
none
Orbus-6E | IUS |
Total mass: 723,490
kg
Payload:
(LEO)
(GSTT) |
14,742 kg
4,990 kg |
Fairing:
|
(42)
(42)
(43) |
- Intelsat-6
- Mars Observer
- Skynet / JCSat |
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Launches: 4 (Failures: 0) /1990-1992/
· PAM-D2 · Orbus-7S
· Orbus-21S
· TOS-21H |
L
1
2
1 |
F |
/1990/
/1990/
/1992/ |
Payload:
(PAM-D2) Skynet 4
(Orbus-7S) JCSat
(Orbus-21S) Intelsat-6
(TOS-21H) Mars Observer |
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Retired |
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Titan 4 (401A) Engines:
0. 2 × UA1207
1. 2 × LR-87-11
2. 1 × LR-91-11 3. 2 × RL-10A-3 | Centaur-T
Total mass: 920,000
kg
Apogee: 40,000 km
Payload:
(GSTT)
(GSO) |
6,350 kg
4,536 kg |
Fairing:
|
(47)
(48) |
- Milstar, Mercury
- Trumpet, Orion |
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Titan 4 (402A) Engines:
0. 2 × UA1207
1. 2 × LR-87-11
2. 1 × LR-91-11
3. 1 × Orbus-21 | IUS
4. 1 × Orbus-6E | IUS
Total mass: 910,000 kg
Apogee: 40,000
km
Payload:
Fairing:
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Titan 4
(403A, 404A, 405A) Engines:
0. 2 × UA1207
1. 2 × LR-87-11
2. 1 × LR-91-11
Total mass: 906,000
kg
Apogee: 1,000 km
Payload:
(LEO)
(SSO) |
17,100 kg
14,090 kg |
Fairing:
|
(44)
(45)
(46) |
- KH-11 (Kennen)
- NOSS, Quasar
- Lacrosse |
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Launches: 22 (Failures: 2) /1989-1998
(401A)
(402A)
(403A-405A) |
L
9
3
10 |
F
1
1 |
/1994-1998/
/1989-1994/
/1990-1997/ |
Payload:
(403A-405A) KH-11 (Kennen / Crystal), Lacrosse, Quasar,
3 × Intruder (NOSS)
+ TLD (Titan Launch Dispenser)
(402A) DSP
(401A) Milstar, Trumpet, Mercury, Orion |
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AJ-23-153 | TLD |
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Retired |
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Titan 4 (403A, 404A, 405A) |
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Titan 4 (401A) Centaur T |
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Titan 4 (402A) IUS |
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Titan 4B
(401B) Engines:
0. 2 × USRM
1. 2 × LR-87-11
2. 1 × LR-91-11
3. 2 × RL-10A-3 | Centaur-T
Total mass: 943,050 kg
Apogee: 40,000
km
Payload:
(GSO)
(IPT) |
5,773 kg
8,600 kg |
Fairing:
|
(46)
(47)
(48) |
- Cassini / Huygens
- Milstar
- Orion |
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Titan 4B (402B) Engines:
0. 2 × USRM
1. 2 × LR-87-11
2. 1 × LR-91-11
3. 1 × Orbus-21 | IUS
4. 1 × Orbus-6E | IUS
Total mass: 925,000 kg
Apogee: 40,000
km
Payload:
Fairing:
|
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Titan 4B
(403B, 404B, 405B) Engines:
0. 2 × USRM
1. 2 × LR-87-11
2. 1 × LR-91-11
Total mass: 910,000 kg
Apogee: 1,000
km
Payload:
(LEO)
(SSO) |
21,900 kg
17,650 kg |
Fairing:
|
(44)
(46) |
- KH-11, Misty
- Onyx |
|
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Launches: 17 (Failures: 2) /1997-2005/
(401B)
(402B)
(403B-405B) |
L
7
5
5 |
F
1
1 |
/1997-2005/
/1997-2004/
/1999-2005/ |
Payload:
(403A-405A) Misty, Onyx, KH-11 (Kennen / Crystal)
(402A) DSP
(401A) Milstar, Orion, Cassini |
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R-4D (Cassini) |
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Retired |
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Titan 4B (403B, 404B, 405B) |
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Titan 4B (401B) Centaur T |
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Titan 4B (402B) IUS |
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Engines:
0. 2 × solid motor
1. 2 × LR-87-7
2. 1 × LR-91-7
Total mass: 388,560 kg
Payload (LEO): 8,030 kg |
 |
Titan Centaur - Dyna Soar |
Engines:
1. 2 × LR-87-5
1. 2 × RL-10A | Centaur
Total mass: 162,000 kg
Payload (LEO): ~ 6,000 kg |
 |
Engines:
0. 2 × UA1205
1. 2 × LR-87-9
2. 1 × LR-91-9
3. 2 × AJ10-138 | Transtage
Total mass: 626,190 kg
Payload (LEO): 13,100 kg |
 |
Never flown |
|
|
 |
Engines:
0. 2 × UA1205
1. 2 × LR-87-11
2. 1 × LR-91-11
3. 2 × AJ10-138 | Transtage
Total mass: 626,190 kg
Payload (LEO): 10,884 kg
Status: Study /1988/
|
 |
Payload:
HL20 / CERV (Crew Emergency Return Vehicle) |
|
 |
Never flown |
|
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|
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Engines:
0. 2 × UA1207
1. 2 × LR-87-11
2. 1 × LR-91-11
3. 2 × AJ10-138 | Transtage
Payload:
(LEO)
(GSTT) |
15,800 kg
4,300 kg |
Status: Study /1965/ |
 |
Engines:
0. 2 × UA1207
1. 2 × LR-87-11
2. 1 × LR-91-11 Payload (LEO): 17,000 kg
Total mass: 836,560 kg
Status: Development
/ended 1967/ |
 |
Never flown |
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Engines:
0. 2 × UA1207
1. 4 × LR-87-11
2. 1 × LR-91-11 Payload (LEO): 22,680 kg
(148 × 240 km, 80 )
Status: Study /1966/ |
 |
Never flown |
 |
Engines:
0. 2 × UA1207
1. 4 × LR-87-11
2. 1 × LR-91-11
3. 2 × RL-10A-3 | Centaur
Total mass: 1,096,920 kg
Payload:
(LEO)
(GSTT) |
25,800 kg
10,430 kg |
Status: Study /1965/ |
 |
Engines:
0. 4 × UA1207
1. 4 × LR-87-11
2. 1 × LR-91-11
3. 2 × RL-10A-3 | Centaur
Total mass: 1,747,580 kg
Payload:
(LEO)
(GSTT) |
36,000 kg
14,515 kg |
Status: Study /1965/ |
 |
Engines:
0. 5 × UA1207
1. 4 × LR-87-11
2. 1 × LR-91-11
Total mass: 2,318,000 kg
Payload:
Fairing:
Status: Study /1986/ |
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Payload:
Zenith Star (space-based chemical laser missile defense weapon) |
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Never flown |
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