This page contains the lift launch systems constructed by some solid fuel stages except final stage.
Vehicle | Stage number | Origin | Manufacturer | Height (meter) | Diameter (meter) | Weight (ton) | Mass to LEO (kg) | Mass to Other Orbit (kg) | Maiden flight | Retired | Record | Status | ASLV | 5 | {{IND}} | ISRO | 24 | 1 | 41 | 150 | 1987 | 1994 | 2/4 | Retired}} |
Epsilon (without PBS) | 3 | {{JPN}} | IHI AeroSpace | 24.4 | 2.6 | 90.8 | 2016 | - | 1/1 | Active}} |
J-I | 2(+1) | {{JPN}} | NASDA / ISAS | 33.1 | 1.8 | 88.5 | 1000 | 1996 | 1996 | 1/1* | Retired}} |
Kaituozhe-1 | 4 | {{CHN}} | CASIC | SSO: 50 | 2002 | ? | 0/2 | {{?}} |
Kaituozhe-2 | {{CHN}} | CASIC | 2017 | 1/1 | Active}} |
Kuaizhou-11 | 4 | {{CHN}} | CASIC | ? | 2.2 | 78 | 1500 | SSO: 1000@700km | 2017 | - | - | Development}} |
L-4S | 4 | {{JPN}} | Tokyo univ. | 16.5 | 0.735 | 9.4 | 26 | 1966 | date=December 2015}} | 1/5 | Retired}} |
Minotaur I | 4 | {{USA}} | Orbital Sciences | 19.2 | 1.67 | 36.2 | 580 | SSO: 331 | 2000 | - | 11/11 | Active}} |
Minotaur IV Lite | 3 | {{USA}} | Orbital Sciences | 23.88{{cn|date=December 2015}} | 2.34{{cn|date=December 2015}} | 86.3{{cn|date=December 2015}} | - | 2010 | - | 2/2* | Active}} |
Minotaur IV | 4 | {{USA}} | Orbital Sciences | 23.88{{cn|date=December 2015}} | 2.34{{cn|date=December 2015}} | 86.3{{cn|date=December 2015}} | 1735{{cn|date=December 2015}} | 2010 | - | 1/1 | Active}} |
Minotaur IV+ | 4 | {{USA}} | Orbital Sciences | 23.88 | 2.34 | 86.3 | 1985 | 2011 | 1/1 | Active}} |
Minotaur IV/Orion 38 | 4 | {{USA}} | Orbital Sciences | 2017 | - | 1/1 | Active}} |
Minotaur V | 5 | {{USA}} | Orbital Sciences | 1.67 | GTO:640 TLI:447 | 2013 | - | 1/1 | Active}} |
M-3C | 3 | {{JPN}} | Tokyo univ. | 20.2 | 1.41 | 41.8 | 195 | 1974 | 1979 | 3/4 | Retired}} |
M-3H | 3 | {{JPN}} | Tokyo univ. | 23.8 | 1.41 | 48.7 | 300 | 1977 | 1978 | 3/3 | Retired}} |
M-3S | 3 | {{JPN}} | Tokyo univ. | 23.8 | 1.41 | 48.7 | 300 | 1980 | 1984 | 4/4 | Retired}} |
M-3SII | 3(+1) | {{JPN}} | ISAS | 27.8 | 1.41 | 61 | 770 | 1985 | 1995 | 7/8 | Retired}} |
M-4S | 4 | {{JPN}} | Tokyo univ. | 23.6 | 1.41 | 43.6 | 180 | 1970 | 1972 | 3/4 | Retired}} |
M-V | 3(+1) | {{JPN}} | ISAS | 30.8 | 2.5 | 140 | 1850 | Interplanetary: 500 | 1997 | 2006 | 6/7 | Retired}} |
Pegasus | 3 | {{USA}} | Orbital Sciences | 16.9 | 1.27 | 18.5 | 375 | 1990 | 10/11 | {{?}} |
Pegasus XL | 3 | {{USA}} | Orbital Sciences | 17.6 | 1.27 | 23.13 | 443 | 1994 | - | 29/32 | Active}} |
Scout | 4(?) | {{USA}} | NACA | 23 | 1.01 | 21.5 | | 1961 | 1994 | Retired}} |
Scout-A | 4 | {{USA}} | NACA | 25 | 1.01 | 17.85 | | Retired}} |
Shavit | 3 | {{ISR}} | IAI | 15.3{{cn|date=December 2015}} | 1.352{{cn|date=December 2015}} | 23.2{{cn|date=December 2015}} | 160{{cn|date=December 2015}} | 1988 | 1990 | 2/2 | Retired}} |
Shavit1 (LK-A) | 3 | {{ISR}} | IAI | 17.2 | 1.352 | 27.3 | 240 | 1995 | 2004 | 2/4 | Retired}} |
Shavit2 (LK-1) | 3 | {{ISR}} | IAI | 19.5{{cn|date=December 2015}} | 1.352{{cn|date=December 2015}} | 31.2{{cn|date=December 2015}} | 350{{cn|date=December 2015}} | 2007 | - | 2/2 | Active}} |
SLV | 4 | {{IND}} | ISRO | 22 | 1 | 17 | 40 | 1979 | 1983 | 3/4 | Retired}} |
RPS-420 | 4 | {{IDN}} | LAPAN | 9.5 | 0.42 | | 50 | (2014) | - | 0/0 | Development}} |
SPARK (Super Strypi) | 3 | {{USA}} | Hawaii, Sandia, Aerojet Rocketdyne | SSO: 250 | 2015 | - | 0/1 | Active}} |
SS-520(3-stage) | 3 | {{JPN}} | ISAS/JAXA | 9.54 | 0.52 | 2.6 | 4 | - | 2017 | - | 1/2 | Active}} |
Start-1 | 4 | {{RUS}} | MIT | 22.7 | 1.61 | 47.2 | 532 | SSO: 167 | 1993 | - | 6/6 | Active}} |
Taiwan SLV | 4 | {{ROC}} | NSPO | 50 | - | - | 0/0 | Development}} |
Taurus | 3+1 | {{USA}} | Orbital Sciences | 27 | 2.35 | 69 | 1259 | SSO: 889 | 1994 | - | 5/6 | {{?}} |
Taurus XL Minotaur-C | 3+1 | {{USA}} | Orbital Sciences | 32 | 2.35 | 77 | 1458 | SSO: 1054 | 2004 | - | 2/4 | Active}} |
VLS-1 | 3 | {{BRA}} | AEB | 19.5{{cn|date=December 2015}} | 1.01{{cn|date=December 2015}} | 50.7{{cn|date=December 2015}} | 380{{cn|date=December 2015}} | 1997 | - | 0/2 | Development}} |