USA

Atlas A

Atlas B

Atlas C

Atlas D

Atlas E / F

Atlas A (XSM-65A)
Engines:

2 × XLR-89-1

Atlas B (XSM-65B)
Engines:

0.
1.

2 × XLR-89-3
1 × XLR-105-3

Atlas C (XSM-65C)
Engines:

0.
1.

2 × XLR-89-5
1 × XLR-105-5

Atlas D (SM-65D)
Engines:

0.
1.

2 × LR-89-5
1 × LR-105-5

Atlas E (SM-65E)
Engines:

0.
1.

2 × LR-89-5
1 × LR-105-5

Atlas F (SM-65F)
Engines:

0.
1.

2 × LR-89-5
1 × LR-105-5

Total mass:
81,647 kg 107,610 kg 110,740 kg 119,000 kg 121,000 kg 121,980 kg 150,540 kg	(A) (B) (C) (D) (E) (F) (H)

Payload:
(LEO)
- 70 kg 70 kg 1,360 kg 820 kg	(A) (B) (C) (D) (E)

Fairing:

(R1)
(0)
(w2)
(w3)
(w4)
(w5)

- RVX (reentry)
- dummy
- Mk.2
- Mk.3
- Mk.4
- Mk.5

Launches: 234 (Failures: 60)
/1957-1974/

(A)
(B)
(C)
(D)
(E)
(F)

L
8
10
6
116
34
55

F
5
3
3
25
13
11

  /1957-1958/
  /1958-1959/
  /1958-1959/
  /1959-1967/
  /1960-1968/
  /1961-1974/

Atlas - NTMP

- RMP

Atlas - ABRES

Atlas - OV1

Atlas - BMRS

Atlas - Trident

Atlas

	Atlas - NTMP / RMP
	Atlas - ABRES / BMRS

Engines:

0.
1.

2 × LR-89-5
1 × LR-105-5

Fairing:

NTMP (Nike target)
	(31, 32) - TVX MP

RMP (Nike-X target)
	(33, 34) - RMV RV

ABRES (reentry)
	(41) - AX (42) - LORV (43) - MTV (44) - REX (45) - WAC (46) - (S)BGRV

BMRS (reentry)
	(47)

	(v0) - suborbital payload

Launches: 106 (Failures: 10)
/1962-1974/

(NTMP)
(RMP)
(ABRES)
(BMRS)

L
35
17
46
8

F
5
2
3

  /1962-1966/
  /1967-1970/
  /1963-1971/
  /1973-1974/

Payload:
(NTMP) Nike Target Measurements Program: TVX MP

(RMP) Nike-X Reentry Measurements Program: RMV (Maneuverable RV), HIRS (High Impulse Retrorocket System),

(ABRES) Advanced Ballistic Reentry Systems: MTV (Material Test Vehicle), LORV (Low Observable RV), (S)BGRV (Simulated Boost Glide RV), REX (Reduced Exoatmospheric Cross Section), WAC (Wake Analisis & Control), AX

(BMRS) Ballistic Missile Reentry Systems: ACE, SFT, RVTO

Atlas D OV1 (x 1 )
Engines:

0.
1.
2.

2 ×  LR-89-3
1 ×  LR-105-3
1 ×  X-258 | 1 × OV1

Fairing:

(w2)
(43)
(v1)

- Mk.2
- MTV
- OV1 (x 1)

Launches: 2 (Failures: 1)
/1965/

Payload: (ABRES)
MTV (Material Test Vehicle)

Retired

Atlas E / F - Trident
Engines:

0.
1.
2.

2 ×  LR-89-5
1 ×  LR-105-5
1 ×  Trident

Fairing:

(51) RMP B
(52) RMP B, ABRES RTVO

Launches: 19 (Failures: 2)
/1967-1971/

Payload: RMP B, ABRES RTVO

Retired

Orbital / without Upper Stage

Atlas D Mercury

Atlas SLV3 Prime

Atlas SLV3 Adta

Atlas B

Atlas B
Engines:

0.
1.

2 × XLR-89-3
1 × XLR-105-3

Atlas SLV3
Engines:

0.
1.

2 × LR-89-5
1 × LR-105-5

Atlas D - Mercury
Engines:

0.
1.

2 × LR-89-5
1 × LR-105-5

Total mass:
107,610 kg 119,000 kg 116,100 kg	(B) (SLV3) (D-Mercury)

Payload:
(LEO)
70 kg 800 kg 1,350 kg	(B) (SLV3) (D-Mercury)

Fairing:

(0)
(1)
(1)

- SCORE
- ADTA
- PRIME

Launches: 15 (Failures: 0)
/1958-1967/

(B)
(SLV3)
(D)

L
1
4
10

F

3

  /1958-1958/
  /1966-1967/
  /1959-1963/

Payload:
(B) SCORE

(SLV3) ADTA,X-23A (SV-5D) PRIME (Precision Reentry Including Maneuvering reEntry)

(D-Mercury) Mercury


	TE-M-316 x 3 (retro motor)

Retired

Atlas C Able

Atlas D Able

Atlas C / D Able
Engines:

0.
1.
2.
3.

2 ×  XLR-89-5
1 ×  XLR-105-5
1 ×  AJ10-101A
1 ×  X-248

Total mass: 120,051 kg

Payload:
(TLT) 170 kg

Fairing:
   (3)

Launches: 4 (Failures: 4)
/1959-1960/

L
1
3

F
1
3

/1959-1959/
/1959-1960/

Payload: Pioneer

Retired

Atlas LV3 Agena A

Atlas LV3 Agena A
Engines:

0.
1.
2.

2 ×  LR-89-5
1 ×  LR-105-5
1 ×  Bell 8048 | Agena A

Total mass: 126,150 kg
Apogee: 600 km
Payload (LEO): 1,250 kg

Fairing:

(4)
(5)

- MIDAS
- Samos

Launches: 4 (Failures: 2)
/1960-1961/

Payload: MIDAS, Samos

Retired

Atlas LV 3 Agena B

Atlas LV3 Agena B
Engines:

0.
1.
2.

2 ×  LR-89-5
1 ×  LR-105-5
1 ×  Bell 8081 | Agena B

Atlas SLV3 Agena BEngines:

0.
1.
2.

2 ×  LR-89-5
1 ×  LR-105-5
1 ×  Bell 8081 | Agena B

Total mass: 130,500 kg
Apogee: 400,000 km

Payload:

(LEO)
(GSTT)

1,725 kg
850 kg

Fairing:

(6)
(7)
(8)
(9)
(10)
(11)

- MIDAS
- Samos-E2
- Samos-E5
- Samos-E6
- OGO
- Ranger, Mariner

Launches: 29 (Failures: 7)
/1961-1966/

(LV3)
(SLV3)

L
28
1

F
7

/1961-1965/
/1966-1966/

Payload:
(LV3) MIDAS, Samos, OGO, Ranger, Mariner

(SLV3) OGO


	BE-3


	?

Retired

Atlas LV 3 Agena D

Atlas SLV 3 Agena D

Atlas LV3 Agena D
Engines:

0.
1.
2.

2 ×  LR-89-5
1 ×  LR-105-5
1 ×  Bell 8096 | Agena D

Atlas SLV3 Agena D
Engines:

0.
1.
2.

2 ×  LR-89-5
1 ×  LR-105-5
1 ×  Bell 8096 | Agena D

Total mass: 131,300 kg
Apogee: 400,000 km

Payload:

(LEO)
(GSTT)

1,825 kg
1,000 kg

Fairing:

(12)
(13)
(14)
(15)
(16)
(10)
(1)

- KH-7 (Gambit-1)
- Snapshot
- Vela
- Mariner, Lunar Orbiter
- RTS (MIDAS)
- ATS
- GATV

Launches: 62 (Failures: 6)
/1963-1967/

(LV3)
(SLV3)

L
15
47

F

6

/1963-1965/
/1964-1967/

Payload:
(LV3) KH-7 (Gambit-1), Mariner, Vela

(SLV3) KH-7 (Gambit-1), RTS (MIDAS), Snapshot, Mariner, Lunar Orbiter, ATS, GATV


	Star-12 (retro motor) SR-28 BE-3A


	R-4D


	SNAP

Retired

Atlas SLV 3A Agena D

Atlas SLV3A Agena D
Engines:

0.
1.
2.

2 ×  LR-89-7
1 ×  LR-105-7
1 ×  Bell 8096 | Agena D

Total mass: 153,365 kg

Payload:
Fairing:

(10)
(17)
(18)

- OGO
- Canyon
- Rhyolite / Aquacade

Launches: 12 (Failures: 1)
/1968-1978/

Payload: OGO, Canyon,
Rhyolite / Aquacade

Retired

Atlas SLV 3B Agena D

Atlas SLV3B Agena D
Engines:

0.
1.
2.

2 ×  LR-89-7
1 ×  LR-105-7
1 ×  Bell 8096 | Agena D

Total mass: 140,000 kg

Fairing:
(22)

Launches: 1 (Failures: 0)
/1966/

Payload: OAO

Retired

Atlas F Agena D

Atlas F Agena D
Engines:

0.
1.
2.

2 ×  LR-89-5
1 ×  LR-105-5
1 ×  Bell 8096 | Agena D

Total mass: 132.000 kg
Payload (LPEO): 2,305 kg

Fairing:
   (19)

Launches: 1 (Failures: 0)
/1978/

Payload: Seasat

Retired

Atlas D Antares-2

Atlas D Fire
Engines:

0.
1.
2.

2 ×  LR-89-3
1 ×  LR-105-3
1 ×  Antares-2 | Fire

Apogee: 837 km

Fairing:

(1)

- FIRE (reentry)

Launches: 2 (Failures: 0)
/1964-1965/

Payload: FIRE (Flight Investigation of Re-Entry)

Retired

Atlas SLV3 Burner-2

Atlas F Burner-2

Atlas F Star-17A

Atlas SLV3 / F Burner
Engines:

0.
1.

2.

2 ×  LR-89-5
1 ×  LR-105-5

1 ×  Star-37B | Burner-2
1 ×  Star-17A

Total mass:
122,300 kg 123,250 kg		(F Star-17A) (F Burner-2)

Payload:
(LPEO) 725 kg (Star-17A)

Launches: 3 (Failures: 2)
/1968-1975/

	L	F
(SLV3)
· Burner-2	1	1	/1968/

(F)
· Burner-2 · Star-17A	1 1	1	/1972/ /1975/

Payload:
(SLV3 Burner-2) Radcat

(F Burner-2) Radsat, Radcat

(F Star-17A) RM 20

Retired

Atlas D OV1

Atlas D OV1
Engines:

0.
1.

2.

2 ×  LR-89-3
1 ×  LR-105-3

1 ×  X-258 | 1 × OV1
2 ×  X-258 | 2 × OV1
3 ×  X-258 | 3 × OV1

Total mass: 117,100 kg

Payload:

(LPEO)

141 kg

Fairing:

(w3)
(43)
(v1)
(v2)

- Mk.3
- ABRES (reentry)
- OV1 (x 1)
- OV1 (x 2)

Launches: 7 (Failures: 2)
/1965-1967/

Payload: OV1 1, ABRES, Mk.3, SSP, SSP, PASCOMSAT, FARO

Retired

Atlas F OV1

Atlas E/F MSD

Atlas E Altair-3A

Atlas E/F Star-37S-ISS

Atlas E/F PTS

Atlas E/F SGS-1

Atlas E SGS-2

Atlas E/F OIS

Atlas E / F with

solid-fuel upper stage

Engines:

0. 1.	2 × LR-89-5 1 × LR-105-5
2.	2 × FW-4S 3 × FW-4S 1 × FW-4D 1 × Star-20 1 × Star-27 1 × Star-37S 1 × Star-37E 1 × Star-37E 1 × Star-48	\| OV1 \| OV1 \| MSD \| Altair-3A \| OIS \| ISS \| PTS \| SGS1 \| SGS2
3.	1 × Star-37E 1 × Star-48	\| SGS1 \| SGS2

Total mass:
122,000 kg 123,500 kg 124,000 kg 126,500 kg	(OV1, OIS, PTS) (ISS) (SGS1) (SGS2)

Payload:
(LPEO)
141 kg 800 kg 870 kg 210 kg	(OV1) (MSD) (OIS) (Altair-3A)

(SSO)
1,100 kg	(ISS)

(MoO)
455 kg	(SGS)

Fairing:

(s11)
(s12)
(s13)
(s14)

OV1
Altair-3A, OIS, ISS
SGS, PTS
MSD

Launches: 43 (Failures: 3)
/1968-1995/

	L	F
· OV1 · MSD · Altair-3A · OIS · ISS · PTS · SGS-1 · SGS-2	4 4 1 2 19 1 8 4	1 1 1	/1968-1971/ /1976-1980/ /1990-1990/ /1979-1985/ /1978-1995/ /1974/ /1977-1981/ /1983-1985/

Payload:

(F ОV1) SPADES, Orbiscal, BMRS-A, LOADS, RTDS, Gridsphere, Mylar Balloon, LCS

(E/F MSD) Parcae (NOSS)

(F PTS) NTS

(E/F OIS) Solwind (OSO), Geosat

(E Altair-3A) Stacksat

(E/F ISS) TIROS N, NOAA, DMSP

(E/F SGS-1) NTS, GPS

(E SGS-2) GPS

Retired

Atlas H MSD

Atlas H MSD
Engines:

0.
1.
2.

2 ×  LR-89-7
1 ×  LR-105-7
1 ×  FW-4D | MSD

Total mass: 133,200 kg
Payload (LEO): 3,630 kg

Fairing:

(s10)

MSD

Launches: 5 (Failures: 0)
/1983-1987/

Payload: Parcae (NOSS)

Retired

Atlas LV 3C Centaur

Atlas LV3C Centaur
Engines:

0.
1.

2.

2 ×  LR-89-7
1 ×  LR-105-5

2 × RL-10A-1 | Centaur A
2 × RL-10A-3 | Centaur B
2 × RL-10A-3 | Centaur C

Total mass: 136,124 kg
Apogee: 400,000 km

Fairing:

(20)
(21)

- Surveyor

Launches: 12 (Failures: 3)
/1962-1967/

	L	F
Centaur
(A) (B) (C) (D)	1 1 3 7	1 2	/1962-1962/ /1983-1983/ /1964-1965/ /1965-1967/

Payload: Surveyor

Star-37 + TD-339 × 3

Retired

Atlas SLV3C Centaur-D

Atlas SLV3D Centaur-D1A

Atlas SLV3C Centaur
Engines:

0.
1.
2.

2 × LR-89-7
1 × LR-105-5
2 × RL-10A-3-1 | D

Atlas SLV3D Centaur
Engines:

0.
1.
2.

2 ×  LR-89-7
1 ×  LR-105-5
2 × RL-10A-3-3  | D1A

Total mass: 166,140

Payload:

(LEO)
3,500 kg	(SLV3C)
5,100 kg	(SLV3D)

(IPT)
1,000 kg	(SLV3C)
590 kg	(SLV3D)

(GSTT)
1,900 kg	(SLV3C)
1,914 kg	(SLV3D)

Fairing:

(21)
(22)
(23)

- Surveyor
- Intelsat-4, Pioneer
- ОАО

Launches: 23 (Failures: 4)
/1967-1975/

	L	F
(SLV3C)	17	3	/1967-1972/
(SLV3D)	6	1	/1963-1975/

Payload:

(SLV3C) Surveyor, Mariner, Pioneer, OAO, ATS, Intelsat-4

(SLV3D) Mariner, Pioneer, Intelsat-4


	Star-37 + TD-339 × 3 Star-37E SR-28-3 SVM-4A


	RS-21

Retired

Atlas SLV3D Centaur-D1AR

Atlas SLV3D Centaur
Engines:

0.
1.
2.

2 ×  LR-89-7
1 ×  LR-105-5
2 × RL-10A-3-3  | D1AR

Payload:

(LEO)
(GSTT)
(IPT)

5,100 kg
1,914 kg
1,179 kg

Fairing:

(24)
(25)
(26)

- Intelsat-4, HEAO
- Comstar, Intelsat-5
- Pioneer-Venus

Launches: 26 (Failures: 6)
/1975-1983/

Payload: Intelsat-4, Intelsat-5, Comstar, HEAO, FLTSATCOM, Pioneer-Venus


	Star-24 Star-37F Star-37FX SVM-4A

Retired

Atlas G Centaur-D1AR

Atlas G Centaur
Engines:

0.
1.
2.

2 × LR-89-7
1 × LR-105-7
2 × RL-10A-3-3 | D1AR

Total mass: 166,140 kg
Apogee: 400,000 km

Payload:

(LEO)
(GSTT)

5,900 kg
2,222 kg

Fairing:

(25)

Launches: 7 (Failures: 2)
/1984-1989/

Payload: Intelsat-5, FLTSATCOM


	Star-37F / XF / FM /

Retired

Atlas 1

Atlas 1
Engines:

0.
1.
2.

2 × LR-89-7
1 × LR-105-7
2 × RL-10A-3 | Centaur I

Total mass: 164,300 kg
Apogee: 400,000 km

Payload:

(LEO)
(GSTT)

5,900 kg
2,234 kg

Fairing:

(25)
(MPF)
(LPF)

Launches: 11 (Failures: 3)
/1990-1997/

Payload: Intelsat-5, UFO, FLTSATCOM, CRRES, BS 3h, Galaxy, GOES, BeppoSAX


	Star-30C


	R-4D

Retired

Atlas 2

Atlas 2A

Atlas 2 / 2A
Engines:

0.
1.

2.

2 ×  LR-89-7
1 ×  LR-105-7

2 × RL-10A-3-3A  | 2
2 × RL-10A-4  | 2A

Total mass: 187,600 kg
Apogee: 400,000 km

Payload:

(LEO)	6,580 kg 7,280 kg	(2) (2A)

(GSTT)	2,810 kg 3,039 kg	(2) (2A)

Fairing:
   (MPF)
   (LPF)

Launches: 33 (Failures:0)
/1991-2002/

	L	F
(2)	10		/1991-1998/
(2A)	23		/1992-2002/

Payload: Intelsat K, Quasar, Inmarsat, DSCS-3, DirecTV, UFO, AMSC, Galaxy, GE, Hot Bird, Eutelsat


	Star-37FM


	LEROS TR-306 S400 R-4D

Retired

Atlas 2AS

Atlas 2AS
Engines:

0.
0.
1.
2.

4 ×  Castor-4A
2 ×  LR-89-7
1 ×  LR-105-7
2 × RL-10A-4  | 2AS

Total mass: 234,000 kg
Apogee: 400,000 km

Payload:

(LEO)	8,610 kg
(GSTT)	3,630 kg

Fairing:
(EPF)

Launches: 30 (Failures: 0)
/1993-2004/

Payload: Intelsat-4,7,8, JCSat, Palapa, , AMC, GE, EchoStar, Eutelsat, Quasar, Superbird, SOHO, Galaxy, Hispasat, EOS-AM 1 (Terra), ICO, Intruder


	LEROS R-4D S400

Retired

Atlas wide body

Engines:

0.
1.
2.

2 ×  LR-89-7
1 ×  H-1D
2 × RL-10  | Centaur

Never flown

RETIRED

Missiles    Early Rockets    Delta    Atlas    Titan    Solid Launchers
Saturn    Space Shuttle    Delta 4    Atlas 3, 5    Vulcan    Falcon    Misc ...
Blue Origin Rockets    Starship    SLS    Unflown