|
|
|
Thor DM18 |
 |
|
|
|
|
|
|
Thor DSV2D |
 |
Thor DSV2E |
 |
Thor DSV2F |
 |
DSV2J |
 |
|
|
|
|
|
 |
Thor DM18 (SM-75)
Engines:
1. 1 × MB-3-1 (DM18)
1 × MB-3-2 (DM18C)
Total mass: 49,800 kg
Maximum range: 2,400 km
Ceiling: 480 km
Fairing:
First launch: 1957
Operational Capability: 1957 |
 |
Launches: 71 (Failures: 21)
/1957-1962/
|
 |
Thor DSV2D / E / F / J Engines:
1. 1 × MB-3-1
Total mass:
50,000 kg (DSV2D)
49,300 kg (DSV2E)
50,000 kg (DSV2F)
55,000 kg (DSV2J)
Fairing:
|
(9)
(w2)
(x1)
(h1)
(h2)
(h3) |
- AVT (Echo balloons)
- Mk.2 (Fishbowl)
- ASV, AEV (ASSET)
- AP (ASAT)
- HAP (ASAT)
- BMDTTP (ASAT) |
|
 |
Launches: 31 (Failures: 5) /1958-1975/
(DSV2D)
(DSV2E)
(DSV2F)
(DSV2J) |
L
2
8
3
18 |
F
4
1 |
/1962-1962/
/1962-1962/
/1963-1964/
/1964-1975/ |
Payload:
(D) AVT (Echo balloons)
(E) Fishbowl (Nuke + Sensors)
(F) ASSET (Aerothermodynamic Elastic Structural Systems Environmental Tests)
(J) ASAT (Anti-satellite weapons) |
|
 |
Retired |
|
|
|
Thor DM18 Able |
 |
|
Thor DM18 Able 1 |
 |
|
|
|
|
Thor DM18 Able 2 |
 |
Thor DM18 Able
2m |
 |
Thor DM18 Able 3 |
 |
|
|
|
Thor DM18 Able 4 |
 |
|
|
|
|
|
 |
Thor Able / Able 2 Engines:
Total mass: 51,608 kg
Fairing:
|
(R3)
(R4) |
Thor Able (reentry)
Thor Able 2 (reentry) |
|
 |
Thor Able 1 / 2 / 3 / 4
Engines:
Total mass: 52,000 kg
Payload (IPT): ~40
kg
Fairing:
|
(p)
(m) |
Thor Able 1, 3, 4
Thor Able 2m |
|
 |
Launches: 16 (Failures: 6) /1958-1960/
|
L |
F |
|
(0)
(1)
(2)
(2m)
(3)
(4) |
3
3
6
2
1
1 |
1
3
1
1 |
/1958-1958/
/1958-1958/
/1959-1959/
/1959-1960/
/1959-1959/
/1960-1960/ |
Payload:
(0) ARTV (reentry)
(1) Pioneer
(2) PGRTV (reentry)
(2m) Transit, TIROS
(3) Explorer
(4) Pioneer |
 |
 |
TX-8 |
|
 |
Retired |
|
|
Thor DM21 Able Star |
 |
Thor DSV2A Able Star 2 |
 |
|
|
|
 |
Thor Able Star Engines:
1. 1 × MB-3-2
2. 1 × AJ10-104
Total mass: 53,000 kg
Payload (LPEO): 150 kg
Fairing: (1) |
 |
Launches: 24 (Failures: 6) /1960-1965/
|
L |
F |
|
(DM21) |
16 |
6 |
/1960-1962/ |
(DSV2A) |
8 |
1 |
/1963-1965/ |
Payload: Transit, Solrad, LOFTI, Injun, TRAAC, ANNA 1, SECOR, Dragsphere, Dodecapole |
|
 |
Retired |
|
|
Thor DM18 Agena A |
 |
|
|
|
 |
Thor Agena A Engines:
1. 1 × MB-3-1
2. 1 × Bell 8048 | Agena A
Total mass: 53,130 kg
Apogee: 1,000 km
Payload (LPEO): 250
kg
Fairing:
|
 |
Launches: 16 (Failures: 6) /1959-1960/
 |
 |
Star-12 (retro motor) |
|
 |
Retired |
|
|
|
Thor DM21 (SLV2) Agena
B |
 |
|
|
|
|
 |
Thor SLV2 Agena B
Engines:
1. 1 × MB-3-3
2. 1 × Bell 8081 | Agena B
Total mass: 56,507 kg
Apogee: 1,000 km
Payload (LPEO): 400 kg
Fairing:
|
(2)
(3)
(4)
(5)
(7)
(8)
(9)
(10) |
- KH-2
- KH-3
- KH-4
- KH-5
- RM (MIDAS)
- ELINT
- Echo
- Nimbus, Alouette |
|
 |
Launches: 40 (Failures: 8) /1960-1963/
Payload: KH-2 (Corona), KH-3 (Corona), KH-4 (Corona), KH-5 (Argon), RM, P-102 (ELINT), Echo 2, Nimbus, Alouette 2, Explorer |
 |
 |
Star-12 (retro motor) |
|
 |
Retired |
|
|
|
|
Thor SLV2A Agena B |
 |
|
|
 |
Thor SLV2A Agena B
| TAT Agena B |
| |
Engines:
0. 3 × Castor-1 | M33-20-4
1. 1 × MB-3-3
2. 1 × Bell 8096 | Agena B
Total mass: 67,500 kg
Apogee: 1,000 km
Payload (LPEO): 400
kg
Fairing:
|
(8)
(10) |
- ELINT
- Nimbus |
|
 |
Launches: 2 (Failures: 0) /1963-1966/
Payload: P-102 (ELINT), Nimbus |
|
 |
Retired |
|
|
Thor SLV2 Agena D |
 |
|
|
|
|
 |
Engines:
1. 1 × MB-3-3
2. 1 × Bell 8096 | Agena D
Total mass: 56,507 kg
Apogee: 1,000 km
Fairing:
|
(4)
(5)
(9)
(12)
(13)
(14) |
- KH-4
- KH-5
- DSAP
- Star Rad
- MPRV
- Poppy |
|
 |
Launches: 22 (Failures: 3) /1962-1967/
Payload: KH-4 (Corona), KH-5 (Argon), Star-Rad, MRPV, DSAP, (Poppy, Timation, Injun 3, Surcal, Calsphere, Wild Bill, LOFTI, Calsphere, NRL-PL 150B, OPS, SECOR) |
 |
 |
Star-12 (retro motor) |
|
 |
Retired |
|
|
Thor SLV2A Agena D |
 |
|
|
|
|
 |
Thor SLV2A Agena D
| TAT Agena D |
| |
Engines:
0. 3 × Castor-1 | M33-20-4
1. 1 × MB-3-3
2. 1 × Bell 8096 | Agena D
Total mass: 67,819 kg
Payload (LPEO):
400
kg
Fairing:
|
(4)
(4A)
(5)
(6)
(7)
(9)
(10)
(14)
(15)
(16) |
- KH-4
- KH-4A
- KH-5
- KH-6
- Quill
- PAGEOS
- OGO
- Poppy
- SAMOS-F3
- SAMOS / ELINT |
|
 |
Launches: 60 (Failures: 4) /1963-1968/
Payload: KH-4 (Corona), KH-4A (Corona), KH-5 (Argon), KH-6 (Lanyard), P-698 (SAMOS), P-770 (SAMOS), Multigroup (ELINT), Quill, OGO, PAGEOS, (Poppy, SECOR, Hayloft) |
 |
 |
Star-12 (retro motor) |
|
 |
Retired |
|
|
|
|
Thorad SLV2G Agena D |
 |
Thorad SLV2H Agena D |
 |
|
|
|
 |
Thorad SLV2A Agena D
| (LT) TAT Agena D |
| |
Engines:
0. 3 × Castor-2
1. 1 × MB-3-3 | LT
2. 1 × Bell 8096 | Agena D
Total mass: 91,400 kg
Apogee: 1,000 km |
 |
Thorad SLV2H Agena D
| (LT) TAT Agena D |
| |
|
Engines:
0. 3 × Castor-2
1. 1 × MB-3-3 | LT
2. 1 × Bell 8096 | Agena D
Apogee: 1,000 km
Fairing:
|
(4a)
(4b)
(10)
(17)
(18) |
- KH-4A
- KH-4B
- OGO, NIMBUS
- Strawman (ELINT)
- Poppy |
|
 |
Launches: 43 (Failures: 2) /1966-1972/
|
L |
F |
|
(SLV2G) |
30 |
1 |
/1966-1971/ |
(SLV2H) |
13 |
1 |
/1969-1972/ |
Payload: KH-4A (Corona), KH-4B (Corona), OGO, Nimbus, Strawman (ELINT), SERT, ASTEX, (Poppy, NRL-PL, Timation, Tempsat, Cylinder, Weston) |
 |
 |
Star-12 (retro motor) |
|
 |
Retired |
|
|
|
Thor LV2D MG 18 |
 |
Thor LV2D Altair-3 |
 |
Thor LV2F Burner-2 |
 |
LV2F Burner-2 Star-13A |
 |
Thor LV2F Burner-2A |
 |
Thor LV2F Star-37XE Star-37S |
 |
|
|
|
 |
Thor Burner Engines:
1. 1 × MB-3-1
2. 1 × MG-18
1 × FW-4S | Altair-3 |
 |
Thor Burner-2
Engines: |
1. |
1 × |
MB-3-1 |
2. |
1 × |
Star-37B | Burner-2 |
|
3. |
1 × |
none
Star-13A |
|
 |
Thor Burner-2A Engines:
1. 1 × MB-3-1
2. 1 × Star-37B | Burner-2
3. 1 × Star-26B |
 |
Thor ISS Engines:
1. 1 × MB-3-1
2. 1 × Star-37XE
3. 1 × Star-37S |
| ISS
| ISS |
Payload (LEO):
55 kg
150 kg
250 kg
300 kg
500 kg |
(FW-4S)
(MG 18)
(Burner-2)
(Burner-2A)
(ISS) |
Fairing:
|
(s1)
(s2)
(s3)
(s4)
(10) |
MG-18
FW-4S
Burner-2
Burner-2A
ISS |
|
|
 |
Launches: 31 (Failures: 3) /1965-1980/ |
|
L
| F |
|
(LV2D) |
· MG-18
· Altair-3 |
2
4 |
1 |
/1965-1965/
/1965-1966/ |
|
(LV2F) |
· Burner-2
· Burner-2A
· ISS |
12
8
5 |
|
/1966-1971/
/1971-1976/
/1976-1980/ |
Payload:
(MG-18) DSAP-1
(Altair-3) DSAP-2, DSAP-3
(Burner-2) DSAP-4, DSAP-5, SESP, Aurora, SECOR
(Burner-2A) DSAP-5B, DSAP-5C
(ISS) DMSP-5D |
|
 |
Retired |
|
|
|
Thor DM18 Delta |
 |
|
|
 |
Engines:
1. 1 × MB-3-3
2. 1 × AJ10-142
3. 1 × X-248 | Altair
Total mass: 54,050 kg
Apogee: 100,000 km
Payload:
(LEO)
(GSTT) |
226 kg
45
kg |
Fairing:
(a)
(m) |
 |
Launches: 12 (Failures: 1) /1960-1962/
Payload: Echo, TIROS, OSO, Ariel, Telstar, Explorer |
|
 |
Retired |
|
|
|
Thor DM21 Delta A |
 |
Thor DM21 Delta B |
 |
|
|
|
|
Thor DSV2A Delta C |
 |
Thor DSV2A Delta C1 |
 |
|
|
|
 |
Delta A Engines:
1. 1 × MB-3-2
2. 1 × AJ10-118
3. 1 × X-248 | Altair
Total mass: 50,756 kg
Apogee: 100,000 km
Payload (LEO: )250 kg |
 |
Delta B / C / C1 Engines:
1. 1 × MB-3-2
2. 1 × AJ10-118D
3. 1 × X-248
1 × X-258
1 × FW-4D |
| Altair
| Altair-2
| Altair-3 |
(B)
(C)
(C1) |
Total mass: 51,285 kg
Apogee: 40,000 km
Payload:
(LEO)
(GSTT) |
370 kg
68
kg
82 kg |
(B)
(C) |
|
|
Fairing:
|
(a)
(b)
(m) |
Delta A, B, C
Delta B
Delta B, C, C1 |
|
 |
Launches: 24 (Failures: 2)
/1962-1969/
(A)
(B)
(C)
(C1) |
L
2
9
11
2 |
F
1
1 |
/1962-1962/
/1962-1964/
/1963-1967/
/1966-1969/ |
Payload:
(A) Explorer
(B) Explorer, Relay, Syncom, Telstar, TIROS
(C) Explorer, TIROS, ESSA, OSO
(C1) Explorer, OSO |
 |
 |
Star-13D |
|
 |
Retired |
|
Thor DSV2G Delta |
 |
|
|
Thor DSV2F |
 |
|
|
|
|
 |
Thor DSV2F Engines:
1. 1 × MB-3-1
Total mass: 50,000 kg |
 |
Thor DSV2G Delta Engines:
1. 1 × MB-3-1
2. 1 × AJ10-118D
Total mass: 55,000
kg |
 |
Launches: 6 (Failures: 1)
/1963-1965/
|
L |
F |
|
(DSV2F) |
3 |
|
/1963/ |
(DSV2G) |
3 |
1 |
/1964-1965/ |
Payload: ASSET-ASV |
|
 |
Retired |
|
|
Delta D |
 |
|
|
|
 |
Delta D Engines:
0. 3 × Castor-2
1. 1 × MB-3-2
2. 1 × AJ10-118D
3. 1 × X-258 | Altair-2
Total mass: 63,966 kg
Payload (GSTT): 104 kg
Fairing: (b) |
 |
Launches: 2 (Failures: 0) /1964-1965/
Payload: Syncom, Intelsat-1 |
 |
 |
Star-13D
SVM-1 |
|
 |
Retired |
|
|
Delta E |
 |
|
|
|
 |
Delta E
Engines:
Total mass: 69,023
kg
Payload:
(LEO)
(LPEO)
(GSTT) |
735 kg
553 kg
150 kg |
Fairing: (10) |
 |
Launches: 6 (Failures: 0)
/1965-1967/
Payload: Explorer, Pioneer, TIROS (ESSA) |
|
 |
Retired |
|
|
Delta E1 |
 |
|
|
|
 |
Delta E1
Engines:
Total mass: 68,000
kg
Payload:
(LEO)
(LPEO)
(GSTT) |
735 kg
205 kg
205 kg |
Fairing: (10) |
 |
Launches: 17 (Failures: 0) /1966-1971/
Payload: Explorer, Pioneer, TIROS (ESSA), Intelsat-2, HEOS, ISIS |
 |
 |
Star-13D
SVM-1 |
|
 |
Retired |
|
|
 |
Engines:
1. 1 × MB-3-3
2. 1 × AJ10-118E
|
3. 1 × X-258
1 × FW-4D |
| Altair-2
| Altair-3 |
Total mass: 63,966 kg
Payload:
(LEO) |
450
kg |
(GSTT) |
104 kg |
Fairing: (10) |
 |
Never flown |
|
|
Delta G |
 |
|
|
 |
Delta G Engines:
0. 3 × Castor-1
1. 1 × MB-3-3
2. 1 × AJ10-118E
Total mass: 55,451 kg
Apogee: 400 km
Payload (LEO): 735
kg
Fairing: (10) |
 |
Launches: 2 (Failures: 0) /1965-1971/
 |
 |
Star-12 (retro motor) |
|
 |
Retired |
|
|
 |
Never flown |
|
|
Delta J |
 |
|
|
|
 |
Delta J Engines:
0. 3 × Castor-1
1. 1 × MB-3-3
2. 1 × AJ10-118E
3. 1 × Star-37D
Total mass: 69,497 kg
Payload (GSTT): 278 kg
Fairing: (10) |
 |
Launches: 1 (Failures: 0) /1969-1969/
 |
 |
Star-17 |
|
 |
Retired |
|
|
 |
Engines:
0. 3 × Castor-2 (K3)
6 × Castor-2 (K6)
9 × Castor-2 (K9)
1. 1 × MB-3-3 | LT
2. 1 × RL-10 |
 |
Never flown |
|
|
Delta L |
 |
|
|
 |
Delta L Engines:
0. 3 × Castor-2
1. 1 × MB-3-3 | LT
2. 1 × AJ10-118E
3. 1 × FW-4D | Altair-3
Total mass: 89,935 kg
Payload (GSTT): 300 kg
Fairing: (10) |
 |
Launches: 2 (Failures: 0) /1969-1972/
|
 |
Retired |
|
|
Delta M |
 |
Delta M6 |
 |
|
|
|
 |
Delta M Engines:
0. 3 × Castor-2 (M)
6 × Castor-2 (M6)
1. 1 × MB-3-3 | LT
2. 1 × AJ10-118E
3. 1 × Star-37D
Total mass:
91,000
kg |
(M) |
|
103,700
kg |
(M6) |
|
|
Payload (GSTT) : |
356
kg |
(M) |
|
454
kg |
(M6) |
|
|
 |
Launches: 13 (Failures: 2) /1968-1971/
(M)
(M6) |
L
12
1 |
F
2 |
/1968-1971/
/1971-1971/ |
Payload:
(M) Intelsat, Skynet, NATO
(M6) Explorer (IMP) |
 |
 |
Star-17A
SVM-2 |
|
 |
Retired |
|
|
N-1 |
 |
|
|
|
 |
N-1 Engines:
0. 3 × Castor-2 | TX-354-3
1. 1 × MB-3-3
2. 1 × AJ10-118E
3. 1 × Star-37N
Total mass: 131,330 kg
Payload (LEO): 1,200 kg |
 |
Launches: 7 (Failures: 1) /1975-1982/
Payload: ETS (Kiku), ISS (Ume), ECS (Ayame) |
 |
 |
SVM-2 |
|
 |
Retired |
|
|
Delta N |
 |
Delta N6 |
 |
|
|
|
 |
Delta N Engines:
0. 3 × Castor-2 (N)
6 × Castor-2 (N6)
1. 1 × MB-3-3 | LT
2. 1 × AJ10-118E
 |
Star-12 (retro motor) |
Total mass: |
90,000
kg |
(N) |
|
102,900
kg |
(N6) |
|
|
Apogee: |
1,500 km |
(N6) |
|
|
Payload: |
(LEO) |
900
kg |
(N) |
|
1,600
kg |
(N6) |
|
Fairing: (10) |
 |
Launches: 9 (Failures: 1) /1968-1972/
(N)
(N6) |
L
6
3 |
F
1 |
/1968-1972/
/1970-1971/ |
Payload:
(N) Biosat, OSO, TD, ESSA
(N6) TIROS-M, NOAA, ITOS |
|
 |
Retired |
|
|
Delta 300 |
 |
Delta 900 |
 |
|
|
|
 |
Delta 0 - - -
Engines: |
0. |
3 ×
9 × |
Castor-2
Castor-2 |
(- 3 - -)
(- 9 - -) |
|
1. |
1 × |
MB-3-3 | LT |
2. |
1 × |
AJ10-118F |
(- - 0 -) |
3. |
|
none |
(- - - 0) |
Total mass: |
90,100
kg |
(0300) |
|
116,500
kg |
(0900) |
|
|
Apogee: |
1,500
km |
(0300) |
|
1,500
km |
(0900) |
|
|
Payload (GSTT): |
635
kg |
(0900) |
|
Fairing: (10) |
 |
Launches: 5 (Failures: 1) /1972-1973/
|
L |
F |
|
(300) |
3 |
1 |
/1972-1973/ |
(900) |
2 |
|
/1972-1972/ |
Payload:
(300) NOAA, ITOS
(900) Landsat, Nimbus |
|
 |
Retired |
|
|
Delta 1900 |
 |
Delta 1604 |
 |
|
|
|
|
 |
Delta 1 - - -
Engines: |
0. |
4 ×
6 ×
9 × |
Castor-2
Castor-2 Castor-2 |
(- 4 - -)
(- 6 - -)
(- 9 - -) |
|
1. |
1 × |
MB-3-3 | ELT |
|
2. |
1 × |
AJ10-118F
TR-201 |
(- - 0 -)
(- - 1 -) |
|
3. |
1 ×
1 × |
none
Star-37D
Star-37E |
(- - - 0)
(- - - 3)
(- - - 4) |
Total mass: |
118,000 kg
130,000 kg
110,000 kg
130,000 kg
130,000 kg
130,286 kg |
(1604)
(1900)
(1410)
(1910)
(1913)
(1914) |
|
Apogee: |
900 km
550 km
200,000 km
400,000 km |
(1410)
(1910)
(1604)
(1913, 1914) |
|
Payload: |
(LEO) 1800
kg (1900) |
(GSTT) 680
kg (1604) |
Fairing:
(10) (- - 0 -)
(20) (- - 1 -)
 |
 |
Star-17 / 17A
FW-5 |
|
|
|
Delta 1410 |
 |
Delta 1910 |
 |
Delta 1913 |
 |
Delta 1914 |
 |
|
|
|
|
 |
Launches: 8 (Failures: 0) /1972-1975/
(1604)
(1900)
(1410)
(1910)
(1913)
(1914) |
L
2
1
1
1
1
2 |
F |
/1972-1973/
/1973-1973/
/1975-1975/
/197-19755/
/1973-1973/
/1972-1973/ |
Payload:
(1410) GEOS
(1604) Explorer (IMP)
(1900) Explorer (AE)
(1910) OSO
(1913) Explorer (RAE)
(1914) Anik |
|
 |
Retired |
|
|
Delta 2310 |
 |
Delta 2313 |
 |
|
|
|
|
 |
Delta 2 - - -
Engines: |
0. |
3 ×
9 × |
Castor-2
Castor-2 |
(- 3 - -)
(- 9 - -) |
|
1. |
1 × |
RS-27 | ELT |
2. |
1 × |
TR-201 |
(- - 1 -) |
|
3. |
1 ×
1 × |
none
Star-37D
Star-37E |
(- - - 0)
(- - - 3)
(- - - 4) |
Total mass: |
107,000 kg
131,000 kg
|
(2310, 2313)
(2910, 2913) |
|
|
Apogee: |
1,500 km
3,000 km
40,000 km
100,000 km
120,000 km |
(2310)
(2910)
(2313)
(2913)
(3924) |
|
|
Payload: |
(LEO) 1,887
kg |
(2910) |
|
|
(GSTT) 500 kg
700
kg 724
kg |
(2313)
(2913)
(2914) |
|
|
 |
Launches: 45 (Failures: 1) /1974-1981/
(2310)
(2313)
(2910)
(2913)
(2914) |
L
3
3
6
2
30 |
F
1 |
/1974-1981/
/1974-1977/
/1975-1978/
/1975-1976/
/1974-1979/ |
|
|
|
Delta 2910 |
 |
Delta 2913 |
 |
Delta 2914 |
 |
|
|
|
|
|
Payload:
(2310) NOAA, Intasat, SME
(2313) Skynet, Sirio
(2910) Landsat, Nimbus, Explorer
(2913) COS B, LAGEOS,
(2914) Westar, SMS, Symphonie, Anik, GOES, CTS, Marisat, NATO, Palapa A, ESA-GEOS, GMS, ISEE, Meteosat, Sakura, IUE, BSE, SCATHA |
 |
 |
Star-24
Star-27
SVM-5 / 6
FW-5 |
 |
 |
|
S400 |
|
 |
Retired |
|
|
N-2 Star-37E |
 |
N-2 |
 |
|
|
|
 |
N-2
Engines: |
0. |
3 × |
Castor-2 |
1. |
1 × |
MB-3-3 | ELT |
2. |
1 × |
AJ10-118FJ |
|
3. |
1 × |
none
Star-37E |
 |
|
|
Star-27 |
Total mass: 132,690
kg
Apogee: 185 km
Payload (LEO): 2,000 kg
|
 |
Launches: 8 (Failures: 0) /2002-2014/
·
· 37E |
L
1
7 |
F |
/1987/
/1981-1986/ |
Payload:
(N-2) MOS (Momo)
(N-2 Star-37E) ETS (Kiku),
GMS (Himawari), CS (Sakura),
BS (Yuri), GMS (Himawari) |
 |
 |
Star-27 |
|
 |
Retired |
|
|
H-1 (9 × Castor-2) |
 |
H-1 (6 × Castor-2) UM-129A |
 |
H-1 (9 × Castor-2) UM-129A |
 |
|
|
|
 |
H-1
Engines: |
0. |
6 ×
9 × |
Castor-2
Castor-2 |
1. |
1 × |
MB-3-3 | ELT |
2. |
1 × |
LE-5 |
|
3. |
1 × |
none
UM-129A |
Payload (LEO): |
3,200 kg |
(9 S0) |
|
Total mass: |
142,260 kg
145,000 kg
142,000 kg |
(9 S0)
(6 S0 / UM)
(9 S0 / UM) |
|
 |
Launches: 9 (Failures: 0) /1986-1991/
· 9 C-2
· 6 C-2 / UM
· 9 C-2 / UM |
L
3
1
5 |
F |
/1986-1990/
/1989/
/1987-1991/ |
Payload: EGS (Ajisai), JAS (Fuji, OSCAR), MABES (Jindai), ETS (Kiku), CS(Sakura), GMS (Himawari),
MOS (Momo), DEBUT (Orizuru), BS (Yuri), JERS (Fuyo) |
 |
 |
Star-30B |
|
|
 |
Retired |
|
|
Delta 3910 |
 |
|
|
|
|
Delta 3 - - -
Engines: |
0. |
9 × |
Castor-4 |
(- 9 - -) |
|
1. |
1 × |
RS-27 | ELT |
|
2. |
1 ×
1 × |
TR-201 AJ10-118K |
(- - 1 -)
(- - 2 -) |
|
3. |
1 ×
1 ×
1 ×
|
none
Star-37D
Star-37E
Star-48B |
(- - - 0)
(- - - 3)
(- - - 4)
(- - - 5) |
Total mass: |
190,000 kg
190,000 kg
185,384 kg
191,600 kg
190,000 kg
191,000 kg
191,600 kg |
(3910)
(3913)
(3914)
(3915)
(3920)
(3924)
(3925) |
|
Apogee: |
1,000 km
25,000 km
40,000 km
40,000 km
120,000 km |
(3920)
(3913)
(3910)
(3920)
(3924) |
|
|
|
Delta 3913 |
 |
Delta 3914 |
 |
Delta 3915 |
 |
|
|
|
Delta 3920 |
 |
Delta 3924 |
 |
Delta 3925 |
 |
|
|
|
|
|
Payload: |
(LEO) |
2,494 kg
3,452 kg |
(3910)
(3920) |
|
(GSTT) |
954 kg
1,154 kg
1,284 kg |
(3914)
(3915)
(3925) |
Fairing:
(20) |
 |
Launches: 38 (Failures: 3) /1980-1989/
(3910)
(3913)
(3914)
(3915)
(3920)
(3924)
(3925) |
L
3
1
13
7
4
4
6 |
F
1
2 |
/1980-1988/
/1981-1981/
/1975-1987/
/1980-1982/
/1982-1989/
/1982-1984/
/1982-1987/ |
Payload:
(3910) SMM, IRAS, PIX 2, TVE
(3913) Explorer (DE)
(3914) Satcom, OTS, Anik B, GOES, Exosat, NATO,
(3915) SBS, Satcom, Westar, Insat,
(3920) Landsat-4, Landsat-5, VSE, Delta-Star
(3924) Satcom, (CCE, IRM, UKS)
(3925) Anik-D, Galaxy, Telstar, Palapa-B |
 |
 |
SVM-7
Star-13B
Star-27
Star-30B / BP |
 |
 |
|
R-4D |
|
 |
Retired |
|
|
Delta 5920 |
 |
|
|
 |
Delta 5 - - -
Engines: |
0. |
9 × |
Castor-4A |
(- 9 - -) |
1. |
1 × |
RS-27 | ELT |
2. |
1 × |
AJ10-118K |
(- - 2 -) |
Total mass: 201,580 kg
Apogee: 185 km
Payload (LEO): 3,848 kg
Fairing: (20) |
 |
Launches: 1 (Failures: 0) /1989-1990/
|
 |
Retired |
|
|
Delta 6920 |
 |
|
|
Delta 6925 |
 |
|
|
|
 |
Delta 6 - - -
Engines: |
0. |
9 × |
Castor-4A |
(- 9 - -) |
1. |
1 × |
RS-27A | EELT |
2. |
1 × |
AJ10-118K |
(- - 2 -) |
|
3. |
1 ×
|
none
Star-48B |
(- - - 0)
(- - - 5) |
Total mas: 219,000 kg
Apogee: |
1,000 km
400,000 km |
(6920)
(6925) |
|
Payload: |
(LEO)
(GSTT) |
3,981
kg (6920)
1,446 kg (6925) |
|
Fairing: |
|
-8
-8
-9.5
-10 |
(6925)
(6920)
(6925)
(6920) |
|
 |
Launches: 17 (Failures: 0) /1989-1992/
(6920)
(6925) |
L
3
14 |
F |
/1990-1992/
/1989-1992/ |
Payload:
(6920) LACE, ROSAT, EUVE
(6925) GPS-2, Palapa B, Marco Polo, Inmarsat-2, Geotail, DUVE |
 |
 |
Star-30B / BP
Star-37XFP |
 |
 |
|
R-4D |
|
 |
Retired |
|
|
|
Delta 7320 |
 |
Delta 7326 |
 |
|
|
|
Delta 7420 |
 |
Delta 7425 |
 |
Delta 7426 |
 |
|
|
|
|
Delta 7925 |
 |
|
|
|
 |
Delta 7 - - - ( Delta 2 )
Engines: |
0. |
3 ×
6 ×
9 × |
GEM-40 GEM-40 GEM-40 |
(- 3 - -)
(- 6 - -)
(- 9 - -) |
|
1. |
1 × |
RS-27A | EELT |
|
2. |
1 × |
AJ10-118K |
(- - 2 -) |
|
3. |
1 ×
1 × |
none
Star-48B
Star-37FM |
(- - - 0)
(- - - 5)
(- - - 6) |
Total mass: |
151,700 kg
151,700 kg
157,000 kg
165,000
kg
170,000
kg
170,000
kg
170,000
kg
232,000
kg
220,000 kg
232,000 kg
231,870 kg
231,900 kg
220,000 kg
231,000 kg |
(7320-10)
(7320-10C)
(7326-9.5)
(7420-10C)
(7425-10)
(7425-9.5)
(7426-9.5)
(7920-10L)
(7920-8)
(7920-10C)
(7925-10)
(7925-10L)
(7925-8)
(7925-9.5) |
|
Apogee: |
1,000 km
1,500 km
400,000 km
400,000 km |
(7- -0)
(7920)
(7- -5)
(7- -6) |
|
Payload: |
(LEO) |
2,703
kg
3,185 kg
5,030 kg |
(7320)
(7420)
(7920) |
|
(GSTT) |
934 kg
1,058 kg
1,110 kg
1;819 kg |
(7326)
(7325)
(7425)
(7925) |
|
|
-10C
-10C
-10C
-10L
-10
-8
-9.5
-9.5
-10C
-9.5
-10C
-10L
-10
-9.5
-8 |
(7320)
(7420)
(7920)
(7920)
(7920)
(7920)
(7326)
(7426)
(7425)
(7425)
(7925)
(7925)
(7925)
(7925)
(7925) |
|
 |
 |
 |
Launches: 132 (Failures: 2) /1995-2018/
(7320)
(7326)
(7420)
(7425)
(7426)
(7920)
(7925) |
L
12
3
14
4
1
29
69 |
F
2 |
/1999-2015/
/1998-2001/
/1998-2018/
/1998-2002/
/1999-1999/
/1995-2018/
/1990-2009/ |
Payload:
(7320) FUSE, EO 1, SAC C, Munin, Quickbird, ICESAT, CHIPSat, Swift, NOAA, Jason, WISE, Aquarius, OCO, (SMAP, ExoCube, GRIFEX, FIREBIRD)
(7326) Deep Space, MIDEX, Genesis
(7420) Globalstar, (CALIPSO, CloudSat), COSMO, GeoEye
(7425) Mars Climate Orbiter, Mars Polar Lander, CONTOUR, MIDEX, ICESAT, ELFIN, SurfSat, CP-7
(7426) Stardust
(7920) Radarsat, Surfsat, × TE, MSX, Iridium, ACE, ARGOS, Oerstedt, Sunsat, Landsat, Jason, EOS-PM, EOS-CHEM, Gravity Probe, NROL-21, WorldView, STSS, STSS-ATRR, (NPP, RAX, DICE, AubieSat, M-Cubed, COVE, E1P, U2), (JPSS, Buccaneer RMM, MiRaTA, EagleSat, RadFxSat, MakerSat)
(7925) GPS-2, NATO, ASC, Satcom, Palapa B, Satcom, DFS-Kopernikus, Galaxy, Wind, Koreasat, NEAR, Polar, Thor, Skynet, Bonum, GeoLITE, MITEx, STEREO, THEMIS, Kepler, Deep Impact, Mars Pathfinder, Mars Odyssey, Mars Global Surveyor, MER (Spirit), Phoenix |
 |
 |
Star-5 × 3
Star-30BP / C / E
Star-37FM / XFP |
 |
 |
|
S400
LEROS
TR-306 |
 |
 |
|
NSTAR |
|
 |
 |
Retired |
|
 |
|
Delta 7920 |
 |
|
|
|
|
Delta 7920H |
 |
|
|
Delta 7925H |
 |
|
|
|
 |
Delta 7 - - - H
Engines: |
0. |
9 × |
GEM-46 |
(- 9 - -) |
1. |
1 × |
RS-27A | EELT |
2. |
1 × |
AJ10-118K |
(- - 2 -) |
|
3. |
1 × |
none
Star-48B |
(- - - 0)
(- - - 5) |
Total mass: |
286,000 kg
286,000 kg |
(7920H)
(7925H) |
|
Payload: |
(LEO) |
6,097 kg
5,097 kg
5,899
kg |
(7920H-9.5)
(7920H-10C)
(7920H-10L) |
|
(GSTT) |
2,169 kg
2,123 kg
2,102
kg |
(7925H-9.5)
(7925H-10C)
(7925H-10L) |
|
(IPT) |
1,508 kg
1,474 kg
1,460 kg |
(7925H-9.5)
(7925H-10C)
(7925H-10L) |
Fairing:
|
-10C
-9.5
-9.5 |
(7920H)
(7920H)
(7925H) |
|
 |
Launches: 6 (Failures: 0) /2003-2011/
(7920H)
(7925H) |
L
3
3 |
F |
/2003-2011/
/2003-2007/ |
Payload:
(7920H) Spitzer, GLAST, GRAIL
(7925H) MER (Opportunity), MESSENGER, Dawn |
|
 |
Retired |
|
|
Delta 8930 |
 |
|
|
 |
Delta 8 - - - ( Delta 3 )
Engines: |
0. |
9 × |
GEM-46 |
(- 9 - -) |
1. |
1 × |
RS-27A |
2. |
1 × |
RL-10B-2 |
(- - 3 -) |
Engines:
Total mass: 301,450 kg
Payload:
(LEO)
(GSTT) |
8,292
kg
1,818 kg |
|
 |
Launches: 3 (Failures: 2) /1998-2000/
Payload: Galaxy, Orion 3, DM-F3 |
|
 |
Retired |
|
|
 |
Engines:
0. 12 × GEM-40
1. 2 × RS-27A | 2 EELT
2. 1 × AJ10-118K
3. none
1 × Star-48B / PAM
|
 |
Never flown |
|
|
 |
Engines:
1. 1 × Castor-120
2. 1 × Castor-120
3. 1 × AJ10-118K |
 |
Engines:
0. 9 × Castor-4B | TX-859
1. 1 × Castor-120
2. 1 × Castor-120
3. 1 × AJ10-118K
4. none
1 × Star-37FM
Total mass: 139.600 kg |
 |
Never flown |
|
|