USA

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:

(w4)
(w6)

- Mk 4
- Mk 6

Launches: 81 (Failures: 15)
/1962-1976/

Titan 2

Titan 2 GLV

Titan 2 GLV

Engines:
1. 2 ×  LR-87-5
2. 1 ×  LR-91-5

Total mass: 150,530 kg

Payload mass:
(LEO) 3,600 kg

Fairing:
   (G) - Gemini

Launches: 12 (Failures: 0)
/1964-1966/

Payload: Gemini

Retired

Titan 2 (23) G

Titan 2 (23) G

Engines:
1. 2 ×  LR-87-5
2. 1 ×  LR-91-5

3.        none
    1 ×  Star-37S
    1 ×  Star-37XFP

Total mass: 150,530 kg

Payload mass:

(LEO)
(LPEO)

3,600 kg
2,177 kg

Fairing:

(26)
(27)

Launches: 13 (Failures: 1)
/1988-2003/

	L	F
· · 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

Retired

Titan 3A

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 mass:
(LEO) 3,175 kg

Fairing:
   (1)

Launches: 4 (Failures: 1)
/1964-1965/

Payload: LES, LCS

Retired

Titan 3B

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 mass:
(LEO) 3,300 kg

Fairing:
   (2)

Launches: 22 (Failures: 1)
/1966-1970/

Payload: KH-8
(Gambit-3 Block 1)

Retired

Titan 3 (23) B

Titan 3 (24) B

Titan 3 (33) B

Titan 3 (34) B

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 mass:
(LEO) 3,300 kg

Titan 3 (24) B

Engines:
1. 2 ×  LR-87-11
2. 1 ×  LR-91-11
3. 1 ×  Bell 8096 | Agena D

Total mass: 170,000
Apogee: 1,000 km

Titan 3 (33) B

Engines:
1. 2 ×  LR-87-11
2. 1 ×  LR-91-11
3. 1 ×  Bell 8096 | Agena D

Total mass: 185,000 kg
Apogee: 40,000 km

Titan 3 (34) B

Engines:
1. 2 ×  LR-87-11
2. 1 ×  LR-91-11
3. 1 ×  Bell 8096 | Agena D

Total mass: 188,520 kg
Apogee: 40,000 km

Payload mass:

(LEO)
(LPEO)

~ 3,500 kg
~ 700 kg

Fairing:

(3)
(31)
(32)

- KH-8 (Gambit-3)
- Quasar
- Jumpseat

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

Retired

Titan 3C

Engines:
0. 2 ×  UA1205
1. 2 ×  LR-87-9
2. 1 ×  LR-91-9
3. 2 ×  AJ10-138  | Transtage

Titan 3 (23) C

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 mass:

(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)

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)

Retired

Titan 3C

Titan 3 (23) C

Titan 3 (23) D

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 mass:

(LEO)
(LPEO)

12,300 kg
10,900 kg

Fairing:

(33)
(34)

- KH-9 (Hexagon)
- KH-11 (Kennen)

Launches: 22 (Failures: 0)
/1971-1982/

Payload: KH-9 (Hexagon),
KH-11 (Kennen / Crystal)

Retired

Titan 3 (34) D

Titan 3 (34) D

Engines:
0. 2 ×  UA1206
1. 2 ×  LR-87-11
2. 1 ×  LR-91-11

3.        none
3. 2 ×  AJ10-138  | Transtage
3. 1 ×  SRM 1 | IUS

4.        none
    1 ×  Orbus-6E | IUS

Total mass:
723,490 kg 720,000 kg 725,000 kg	(34D) (34D Transtage) (34D IUS)

Apogee:
185 km 40,000 km 40,000 km	(34D) (34D Transtage) (34D IUS)

Payload mass:

(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

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

Retired

Titan 3 (23) E

Titan 3 (23) E

Engines:
0. 2 ×  UA1205
1. 2 ×  LR-87-11
2. 1 ×  LR-91-11
3. 2 × RL-10A-3 | Centaur

4.        none
    1 ×  Star-37E

Total mass: 632,970 kg
Apogee: 400,000 km

Payload mass:

(LEO)
(GSTT)
(GSO)
(IPT)

17,000 kg
6,800 kg
3,200 kg
5,000 kg

Fairing:
(41)

Launches: 7 (Failures: 1)
/1974-1977/

Payload: Sphinx, Viking,
Helios, Voyager

Retired

Commercial Titan 3 (34)

Engines:
0. 2 ×  UA1206
1. 2 ×  LR-87-11
2. 1 ×  LR-91-11

3.        none
3. 1 ×  Orbus-21S
3. 1 ×  Orbus-21H | TOS-21H
3. 1 ×  Star-63 | PAM-D2

Total mass: 723,490 kg

Payload mass:

(LEO)
(GSTT)

14,742 kg
4,990 kg

Fairing:

(42)
(42)
(43)

- Intelsat-6
- Mars Observer
- Skynet / JCSat

Launches: 4 (Failures: 0)
/1990-1992/

· PAM-D2 · Orbus-7S
· Orbus-21S
· TOS-21H

L
1
2
1

/1990/
/1990/
/1992/

Payload:

(PAM-D2) Skynet 4

(Orbus-7S) JCSat

(Orbus-21S) Intelsat-6

(TOS-21H) Mars Observer

Retired

Commercial Titan 3

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 mass:

(GSTT)
(GSO)

6,350 kg
4,536 kg

Fairing:

(47)
(48)

- Milstar, Mercury
- Trumpet, Orion

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 mass:

(GSTT)

4,944 kg

Fairing:

(45)

- DSP

Titan 4
(403A, 404A, 405A)

Engines:
0. 2 ×  UA1207
1. 2 ×  LR-87-11
2. 1 ×  LR-91-11

4.        none
3. 1 ×  AJ-23-153 | TLD

Total mass: 906,000 kg
Apogee: 1,000 km

Payload mass:

(LEO)
(SSO)

17,100 kg
14,090 kg

Fairing:

(44)
(45)
(46)

- KH-11 (Kennen)
- NOSS, Quasar
- Lacrosse

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

Retired

Titan 4 (403A, 404A, 405A)

Titan 4 (401A) Centaur T

Titan 4 (402A) IUS

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 mass:

(GSO)
(IPT)

5,773 kg
8,600 kg

Fairing:

(46)
(47)
(48)

- Cassini / Huygens
- Milstar
- Orion

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 mass:

(GSO)

2,860 kg

Fairing:

(45)

- DSP

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 mass:

(LEO)
(SSO)

21,900 kg
17,650 kg

Fairing:

(44)
(46)

- KH-11, Misty
- Onyx

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

Retired

Titan 4B (403B, 404B, 405B)

Titan 4B (401B) Centaur T

Titan 4B (402B) IUS

Titan 2 - Dyna Soar

Engines:
1. 2 ×  LR-87-5
2. 1 ×  LR-91-5

Total mass: 150,530 kg

Soltan- Dyna Soar

Engines:
0. 2 ×  solid motor
1. 2 ×  LR-87-7
2. 1 ×  LR-91-7

Total mass: 388,560 kg

Payload mass:
(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 mass:
(LEO) ~ 6,000 kg

Titan 3C - Dyna Soar

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 mass:
(LEO) 13,100 kg

Payload:
Dyna Soar

Never flown

Titan 3 (23) C - HL20

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 mass:
(LEO) 10,884 kg

Status: Study  /1988/