ORBITAL AND PLANETARY LAUNCH SERVICES
The following data comes from _International Reference Guide to Space Launch
Systems_ by Steven J. Isakowitz, 1991 edition.
Notes:
* Unless otherwise specified, LEO and polar paylaods are for a 100 nm
orbit.
* Reliablity data includes launches through Dec, 1990. Reliabity for a
familiy of vehicles includes launches by types no longer built when
applicable
* Prices are in millions of 1990 $US and are subject to change.
* Only operational vehicle families are included. Individual vehicles
which have not yet flown are marked by an asterisk (*) If a vehicle
had first launch after publication of my data, it may still be
marked with an asterisk.
Vehicle | Payload kg (lbs) | Reliability | Price | Launch Site
(nation) | LEO Polar GTO | | | (Lat. & Long.)
-------------------------------------------------------------------------------
-
Ariane 35/40 87.5% Kourou
(ESA) (5.2 N, 52.8 W)
AR40 4,900 3,900 1,900 1/1 $65m
(10,800) (8,580) (4,190)
AR42P 6,100 4,800 2,600 1/1 $67m
(13,400) (10,600) (5,730)
AR44P 6,900 5,500 3,000 0/0 ? $70m
(15,200) (12,100) (6,610)
AR42L 7,400 5,900 3,200 0/0 ? $90m
(16,300) (13,000) (7,050)
AR44LP 8,300 6,600 3,700 6/6 $95m
(18,300) (14,500) (8,160)
AR44L 9,600 7,700 4,200 3/4 $115m
(21,100) (16,900) (9,260)
* AR5 18,000 ??? 6,800 0/0 $105m
(39,600) (15,000)
[300nm]
Atlas 213/245 86.9% Cape Canaveral
(USA) (28.5 N, 81.0W)
Atlas E -- 820 -- 15/17 $45m Vandeberg AFB
(1,800) (34.7 N, 120.6W)
Atlas I 5,580 4,670 2,250 1/1 $70m
(12,300) (10,300) (4,950)
Atlas II 6,395 5,400 2,680 0/0 $75m
(14,100) (11,900) (5,900)
Atlas IIA 6,760 5,715 2,810 0/0 $85m
(14,900) (12,600) (6,200)
* Atlas IIAS 8,390 6,805 3,490 0/0 $115m
(18,500) (15,000) (7,700)
Delta 189/201 94.0% Cape Canaveral
(USA) Vandenberg AFB
Delta 6925 3,900 2,950 1,450 14/14 $45m
(8,780) (6,490) (3,190)
Delta 7925 5,045 3,830 1,820 1/1 $50m
(11,100) (8,420) (2,000)
Energia 2/2 100% Baikonur
(Russia) (45.6 N 63.4 E)
Energia 88,000 80,000 ??? 2/2 $110m
(194,000) (176,000)
H series 22/22 100% Tangeshima
(Japan) (30.2 N 130.6 E)
* H-2 10,500 6,600 4,000 0/0 $110m
(23,000) (14,500) (8,800)
Kosmos 371/377 98.4% Plestek
(Russia) (62.8 N 40.1 E)
Kosmos 1100 - 1350 (2300 - 3000) $??? Kapustin Yar
[400 km orbit ??? inclination] (48.4 N 45.8 E)
Long March 23/25 92.0% Jiquan SLC
(China) (41 N 100 E)
* CZ-1D 720 ??? 200 0/0 $10m Xichang SLC
(1,590) (440) (28 N 102 E)
Taiyuan SLC
CZ-2C 3,200 1,750 1,000 12/12 $20m (41 N 100 E)
(7,040) (3,860) (2,200)
CZ-2E 9,200 ??? 3,370 1/1 $40m
(20,300) (7,430)
* CZ-2E/HO 13,600 ??? 4,500 0/0 $???
(29,900) (9,900)
CZ-3 ??? ??? 1,400 6/7 $33m
(3,100)
* CZ-3A ??? ??? 2,500 0/0 $???m
(5,500)
CZ-4 4,000 ??? 1,100 2/2 $???m
(8,800) (2,430)
Pegasus/Taurus 2/2 100% Peg: B-52/L1011
(USA) Taur: Canaveral
Pegasus 455 365 125 2/2 $10m or Vandenberg
(1,000) (800) (275)
* Taurus 1,450 1,180 375 0/0 $15m
(3,200) (2,600) (830)
Proton 164/187 87.7% Baikonour
(Russia)
Proton 20,000 ??? 5,500 164/187 $35-70m
(44,100) (12,200)
SCOUT 99/113 87.6% Vandenberg AFB
(USA) Wallops FF
SCOUT G-1 270 210 54 13/13 $12m (37.9 N 75.4 W)
(600) (460) (120) San Marco
(2.9 S 40.3 E)
* Enhanced SCOUT 525 372 110 0/0 $15m
(1,160) (820) (240)
Shavit 2/2 100% Palmachim AFB
(Israel) ( ~31 N)
Shavit ??? 160 ??? 2/2 $22m
(350)
Space Shuttle 37/38 97.4% Kennedy Space
(USA) Center
Shuttle/SRB 23,500 ??? 5,900 37/38 $248m (28.5 N 81.0 W)
(51,800) (13,000) [FY88]
* Shuttle/ASRM 27,100 ??? ??? 0/0
(59,800)
SLV 2/6 33.3% SHAR Center
(India) (400km) (900km polar) (13.9 N 80.4 E)
ASLV 150 ??? ??? 0/2 $???m
(330)
* PSLV 3,000 1,000 450 0/0 $???m
(6,600) (2,200) (990)
* GSLV 8,000 ??? 2,500 0/0 $???m
(17,600) (5,500)
Titan 160/172 93.0% Cape Canaveral
(USA) Vandenberg
Titan II ??? 1,905 ??? 2/2 $43m
(4,200)
Titan III 14,515 ??? 5,000 2/3 $140m
(32,000) (11,000)
Titan IV/SRM 17,700 14,100 6,350 3/3 $154m-$227m
(39,000) (31,100) (14,000)
Titan IV/SRMU 21,640 18,600 8,620 0/0 $???m
(47,700) (41,000) (19,000)
Vostok 1358/1401 96.9% Baikonur
(Russia) [650km] Plesetsk
Vostok 4,730 1,840 ??? ?/149 $14m
(10,400) (4,060)
Soyuz 7,000 ??? ??? ?/944 $15m
(15,400)
Molniya 1500kg (3300 lbs) in ?/258 $???M
Highly eliptical orbit
Zenit 12/13 92.3% Baikonur
(Russia)
Zenit 13,740 11,380 4,300 12/13 $65m
(30,300) (25,090) (9,480)