 |
|
|
|
|
|
  |
Scout
|
| |
1. |
2. |
3. |
4. |
5. |
| Engines: Algol |
Castor |
Antares |
Altair |
|
| |
|
|
|
| Blue Scout |
1 |
|
-1B |
-1A |
-1A |
|
|
|
|
| |
2 |
|
-1B |
-1A |
-1A |
-1A |
|
| |
|
|
|
| Scout |
X |
|
-1A |
|
-1A |
|
|
|
|
| |
X |
-1 |
-1B |
-1A |
-1A |
-1A |
|
|
|
|
| |
X |
-1 |
-1C |
-1A |
-1A |
-1A |
|
|
|
|
| |
X |
-1A |
-1C |
-1A |
-1A |
-1A |
+ |
| |
|
|
|
| Scout |
X |
-2 |
-1C |
-1A |
-2A |
-1A |
|
|
|
| |
X |
-2 |
-1D |
-1A |
-2A |
-1A |
|
|
|
| |
X |
-2B |
-1D |
-1A |
-2A |
-2A |
|
|
|
| |
X |
-2M |
-1D |
-1A |
-2A |
MG-18 |
|
| |
|
|
|
| Scout |
X |
-3 |
-2A |
-1A |
-2A |
-1A |
|
|
|
| |
X |
-3A |
-2A |
-1A |
-2A |
-1A |
+ |
|
|
| |
X |
-3C |
-2A |
-1A |
-2A |
|
|
|
|
| |
X |
-3M |
-2A |
1A |
-2A |
MG-18 |
|
|
|
| |
X |
-4 |
-2A |
-1A |
-2A |
-2A |
|
|
|
| |
X |
-4 |
-2B |
-1A |
-2A |
-2A |
|
|
|
| |
X |
-4A |
-2B |
-1A |
-2A |
-2A |
+ |
|
|
| |
X |
-5C |
-2B |
-2A |
-2A |
|
|
| |
|
|
|
| Scout |
A |
|
-2B |
-2A |
-2A |
-2A |
|
|
|
| |
A |
-1 |
-2C |
-2A |
-2A |
-2A |
|
|
|
| |
B |
|
-2B |
-2A |
-2A |
-3 |
|
|
|
| |
B |
-1 |
-2C |
-2A |
-2A |
-3 |
|
| |
|
|
|
| Scout |
D |
-1 |
-3A |
-2A |
-2A |
-3A |
|
|
|
| |
E |
-1 |
-3A |
-2A |
-2B |
-3 |
+ |
|
|
| |
F |
-1 |
-3A |
-2A |
-2B |
-3A |
|
|
|
| |
G |
-1 |
-3A |
-2A |
-3A |
-3A |
|
|
| |
|
|
5. |
|
|
|
|
| Scout X-1A / -3A / X |
-4A |
+ NOTS-17 |
| |
E |
-1 |
+ Alcyone-1A |
|
|
| Blue Scout 1 |
 |
| Blue Scout 2 |
 |
| Scout X, X-1 / 2 / 3 / 4 / 5 |
|
| |
|
| X-3C, X-5C |
|
|
|
|
|
|
| A, A-1 |
|
| B, B-1 |
|
| D-1 |
|
| E-1 |
|
| F-1 |
|
| G-1 |
|
|
|
Total mass: 16,000-21,000 kg
Apogee (max): 130,000
km
Payload mass: 59-185 kg |
 |
Launches: 125 (Failures: 20)
/1960-1994/
| |
|
|
L |
|
F |
|
| Blue Scout |
(-1)
(-2) |
|
3
3 |
|
1 |
/1961-1962/
/1961/ |
| |
| Scout |
(X
(X
(X
(X
(X
(X
(X
(X
(X
(X
(X
(X
(X
(
(A
(A
(B
(B
(
(D
(E
(F
(G |
)
-1)
-1A}
-2)
-2B)
-2M)
-3)
-3A)
-3C)
-3M)
-4)
-4A)
-5C)
)
-1)
)
-1)
-1)
-1)
-1)
-1) |
|
1
7
1
2
1
3
6
2
1
1
13
2
1
11
1
25
5
15
1
2
18 |
|
1
4
1
1
2
1
2
1
4
1
1 |
/1960/
/1960-1961/
/1962/
/1962/
/1963/
/1962/
/1962-1964/
/1962-1963/
/1964/
/1963/
/1963-1965/
/1964-1966/
/1968/
/1965-1970/
/1973/
/1965-1971/
/1971-1976/
/1972-1979/
/1974/
/1975/
/1979-1994/ |
Payload: Explorer, USAF Rad Probe, Mercury Scout, P 21A, USAF Reentry Test, Poppy, DSAP, Transit, GRS, Ariel, ESRS, SERT, RFD, San Marco, SECOR, FR, OV3, San Marco, ESRO, Transit, RAM, Azur, OFO, PAET, Eole, BIC, Triad, Aeros, Miranda, ANS, Wideband, GP (Gravity Probe), Transat, HCMM, SAGE, Magsat, Nova, HILAT,, Polar Bear, MACSAT, REX, SAMPEX, MSTI, Radcal
|
|
|
 |
Retired |
|
|
|
|
|
|
|
| Conestoga 1620 |
|
|
|
|
|
Conestoga
Engines (1620):
1. 2 × Castor-4B
2 × Castor-4A
2. 2 × Castor-4B
3. 1 × Castor-4B
4. 1 × Star-48V
Payload mass:
(LEO) 1,179 kg (1620) |
|
Launches: 1 (Failures: 1)
/1995/
|
|
Retired |
|
|
|
| Pegasus |
|
| Pegasus HAPS |
|
| Pegasus H |
|
|
|
|
|
| Pegasus XL |
|
| Pegasus XL
HAPS |
|
|
|
|
|
| Pegasus HXLV |
 |
|
|
|
|
|
Pegasus
Engines:
0. B-52 / L-1011 (aircraft)
1. 1 × Orion-50S
1 × Orion-50SXL
2. 1 × Orion-50
1 × Orion-50XL
3. 1 × Orion-38
4. 1 × MR-107K | HAPS
| Total mass: |
19,000 kg
18,500 kg
24,000 kg
23,000 kg |
(·)
(· H)
(· L)
(· L HAPS) |
|
| |
| Apogee: |
200 km
4,000 km
185 km
4,000 km |
(·)
(· H)
(· L)
(· L HAPS) |
|
| |
| Payload mass: |
| (LEO) |
400 kg
425 kg
400 kg
475 kg
500 kg |
(·)
(· HAPS)
(· H)
(· L)
(· L HAPS) |
|
| |
| (GSTT) |
| 125 kg |
(·) |
|
|
|
|
Launches: 45 (Failures: 5)
/1990-2013/
·
· HAPS
· H
· X
· XL HAPS |
L
4
2
4
29
6 |
F
2
3 |
/1990-1994/
/1991-1994/
/1995-2000/
/1994-2019/
/1997-2005/
|
Payload: SECS, Pegsat, SCD, Orbcomm-CDS, ALEXIS, APEX
(HAPS) Microsat, STEP
(H) Microsat, Orbcomm, MSTI, SCD, Microstar, HETE
(XL) REX, Orbcomm, Eagle, Microstar, STEP, TOMS-EP, FAST, HETE, SAC-B, CPAC, Minisat, Orbview-2, FORTE, SNOE, Teledesic, TRACE, SWAS, WIRE, TERRIERS, SA-200, Orbview, HESSI, SORCE, Galex, SCISAT, ST5, RS-300, C/NOFS, IRIS Interface Region Imaging Spectrograph. Projects: SAC, Small Explorer, STEDI, ICON (MIDEX), Odyssey (USA)
(XL HAPS) Orbcomm, TERRIERS, MUBLCOM, DART
(HXLV) X-43A (Hyper-X) |
|
 |
In service |
|
|
|
|
| Minotaur |
|
|
|
|
|
Minotaur
Engines:
1. 1 × M-55 | Minuteman-1
2. 1 × SR-19 | Minuteman-2
3. 1 × Orion-50XL
4. 1 × Orion-38
5. 1 × MR-107K | HAPS
Total mass: 36,200
kg
Payload mass:
(LEO)
(GSTT) |
640 kg
335 kg |
|
|
Launches: 12 (Failures: 0)
/2000-2021/
|
Payload: Astro-200, ORS-3, RPP, Streak, Microstar, ASUSAT, FalconSat, JAK, JAWSAT, MEMS, OCSE, OPAL, STENSAT, SA-200, Picosat, × SS, Cubesat, USA 185, Genesat, Tacsat ORS, USA (NROL) |
|
|
Retired |
|
|
|
|
|
|
| Minotaur 4 |
|
|
|
|
|
| Minotaur 5 |
|
|
|
|
| |
Engines:
1. 1 × TU-903 (SR-118)
2. 1 × SR-119
3. 1 × SR-120
| 4. |
3 × MR-107K
none
1 × Orion-38
1 × Orion-38
1 × Orion-38
1 × Star-48V
1 × Star-48V
1 × Star-48V |
(3)
(4-Lite)
(4)
(4 HAPS)
(4 Orion-38)
(4+)
(5 (1))
(5 (2)) |
| |
| 5. |
1 × MR-107K
1 × Orion-38
1 × Star-37FM |
(4 HAPS)
(4 Orion-38)
(5) |
Total mass: 36,200
kg
Payload mass:
| (LEO) |
1,720 kg |
(185 km, 28,5 ) |
| (GSTT) |
678 kg |
(5) |
|
|
Launches: 8 (Failures: 0)
/2010-2020/
| |
L |
F |
|
(4)
· Lite
·
· HAPS
· Orion-38
· +
(5)
·
|
2
2
1
1
1
1 |
|
/2010-2011/
/2010/
/2010-2020/
/2017/
/2011/
/2013/ |
Payload:
(4 Lite) HTV
(4) SBSS, USA
(4 HAPS) (STPSat, FASTRAC, FalconSat, RAX, OREOS, NanoSail-D2B)
(4 Orion-38) ORS, DHFR, Prometheus, Prometheus
(4+) TacSat
(5) LADEE |
|
|
In service |
|
|
|
|
| Minotaur 4 ABT |
|
|
|
|
 |
Minotaur 4 ABT
Engines:
1. 1 × TU-903 (SR-118)
|
|
Launches: 1 (Failures: 0)
/2019/
|
Payload: Orion boilerplate capsule |
|
|
Retired |
|
|
|
|
| Athena 1 |
|
|
|
|
|
| Athena 2 |
|
|
|
|
Athena 1
Engines:
1. 1 × Castor-120
2. 1 × Orbus-21D
1 × Orbus-30 (C)
3. 4 × MR-107K | OAM
Total mass: 66,300
kg
Payload mass:
(LEO)
(LPEO) |
795 kg
515 kg |
|
|
Athena 2
Engines:
1. 1 × Castor-120
2. 1 × Castor-120
3. 1 × Orbus-21D
1 × Orbus-30 (C)
4. 4 × MR-107K | OAM
Total mass: 120,700
kg
Payload mass:
(LEO)
(LPEO)
(GSTT) |
1,985 kg
1,490 kg
593 kg |
|
|
Launches: 7 (Failures: 2)
/1995-2001/
|
L |
F
|
|
(1)
(2)
|
4
3 |
1
1 |
/1995-2001/
/1998-1999/ |
Payload:
(1) GemStar, Lewis, ROCSAT, (Starshine, PICOSat, PCSat, SAPPHIRE
(2) Lunar Prospector, Ikonos |
|
|
Retired |
|
|
|
| Taurus L1110 |
|
|
|
|
|
| Com. Taurus L2110 |
|
| Com. Taurus L2210 |
|
|
|
|
|
| Taurus XL L3110 |
|
| Taurus XL L3210 |
|
|
|
|
|
Taurus 1 - - -
Engines:
1. 1 × TU-903 (SR-118)
2. 1 × Orion-50ST
3. 1 × Orion-50T
4. 1 × Orion-38 |
|
Taurus 2 - - -
Engines:
1. 1 × Castor-120
2. 1 × Orion-50ST
3. 1 × Orion-50T
4. 1 × Orion-38 |
|
Taurus 3 - - -
Engines:
1. 1 × Castor-120
2. 1 × Orion-50SXLT
3. 1 × Orion-50XLT
4. 1 × Orion-38 |
Total mass:
69,000-76,950
kg
| Payload mass: |
| (LEO) |
1,180 kg
1,250 kg
1,050 kg
1,450 kg
1,275 kg |
(1110)
(2110)
(2210)
(3110)
(3210) |
|
| |
| (LPEO) |
1,160 kg
1,180 kg
1,180 kg
925 kg |
(1110)
(2110)
(2210)
(3110) |
|
| |
| (SSO) |
900 kg
900 kg
700 kg
1,050 kg
880 kg |
(1110)
(2110)
(2210)
(3110)
(3210) |
|
| |
| (GSTT) |
370 kg
375 kg
445 kg |
(1110)
(2110)
(3110) |
|
| |
| (IPT) |
295 kg
295 kg |
(3110)
(3210) |
|
Fairing:
| |
(1)
(2)
|
(- 1 - -)
(- 2 - -)
|
|
|
Launches: 10 (Failures: 3)
/1994-2017/
| |
L |
F |
|
| ARPA |
| (L1110) |
3 |
|
/1994-2000/ |
| |
| Commercial Taurus |
(L2110)
(L2210) |
2
1 |
1 |
/1999-2001/
/1998/ |
| |
| Taurus-XL |
(L3110)
(L3210) |
2
2 |
2 |
/2000-2011/
/2004-2017/ |
Payload:
(1000) STEP, DARPASAT, STEX, ATEx, MTI
(2000) KOMPSat, ACRIMSat, Celestis, OrbView, QuikTOMS, SBD
(3000) GFO, Orbcomm, Celestis, OCO, Glory, E1P, KySat, Hermes, ROCSAT, SkySat |
|
|
Retired |
|
|
|
| Super Strypi |
|
|
|
|
Super Strypi (SPARK)
Engines:
1. 1 × LEO-46
2. 1 × LEO-7
3. 1 × LEO-1
Total mass: 27,000
kg
Payload mass:
(LEO)
(SSO) |
300 kg
250 kg |
|
|
Launches: 1 (Failures: 1)
/2015/
|
Payload: HiakaSat, Supernova-Beta, STACEM , EDSN |
|
|
Retired |
|
|
