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LAUNCHER COMPANIES / TRÄGERRAKETENHERSTELLER



Arianespace

Evry, Frankreich

Ariane 40 - 2100 kg GTO
Ariane 42P - 2920 kg GTO
Ariane 44P - 3380 kg GTO
Ariane 42L - 3450 kg GTO
Ariane 44LP - 4170 kg GTO
Ariane 44L - 4700 kg GTO (Startkosten 90 -110 Mio. US-Dollar)
Ariane 5 - 6800 kg GTO



Boeing North American

Downey, Kalifornien, USA

Space Shuttle - 24950 kg LEO (Startkosten 175 - 363 Mio. US-Dollar)



Boeing

Huntington Beach, Kalifornien, USA

Delta 2-7920 - 5136 kg LEO
Delta 2-7425 - 1127 kg LEO
Delta 2-7925 - 1799 GTO (Startkosten 45 - 50 Mio. US-Dollar)
Delta 3 - 3810 kg GTO
Sea Launch/Zenit 3 - 6900 kg GTO (Startkosten 50 - 70 Mio. US-Dollar)



Central Specialized Design Bureau

Samara, Rußland

Sojus U/U2 - 7500 kg LEO
Molnija M/SL-6 - 1600 kg



China Great Wall Industry

Bejing, Volksrepublik China

Langer Marsch 1D - 1000 kg LEO
Langer Marsch 2C - 2500 kg LEO
Langer Marsch 2D - 3300 kg LEO
Langer Marsch 2E - 2490 kg GTO
Langer Marsch 3 - 1400 kg GTO (Startkosten 45 - 70 Mio. US-Dollar)
Langer Marsch 3A - 2500 kg GTO
Langer Marsch 3B - 4800 kg GTO
Langer Marsch 3C - 3700 kg GTO
Langer Marsch 4 - 4000 kg LEO



EER Systems

Seabrook, Maryland, USA

Conestoga 1229 - 300 kg LEO



Eurockot

Bremen, Bundesrepublik Deutschland

Eurockot - 1850 kg LEO



Instituto de Aeronautica e Espaco

Sao Paulo, Brasilien

VLS (Veiculo Lancador de Satellites) - 2000 kg LEO



Israel Aircraft Industries

Yehud, Israel

Shavit - 150 kg LEO



ISRO (Indian Space Research Organisation)

Trivandrum, Indien

ASLV (Augmented Satellite Launch Vehicle) - 150 kg LEO
PSLV (Polar Satellite Launch Vehicle) - 448 kg GTO
GSLV (Geosationary Satellite Launch Vehicle) - 2500 kg GTO



KB Poljot

Omsk, Rußland

Kosmos 3M/SL-6 - 1700 kg LEO



Khrunichev State Research and Production Space Center

Moskau, Rußland

Proton K/SL-12 - 2600 kg GEO (50 - 70 Mio. US-Dollar)
Proton K/SL-13 - 21000 kg LEO
Rockot - 4180 kg LEO



Kistler Aerospace

Kirkland, Washington, USA

K-1 - 3170 kg LEO



Komplex Scientific and Technical Center

Rußland

Start 1 - 500 kg LEO
Start - 700 kg LEO



Lockheed Martin Missiles & Space Company

Sunnyvale, Kalifornien, USA

Athena 1 (LMLV 1) - 800 kg LEO
Athena 2 (LMLV 2) - 2000 kg LEO
Titan 2 - 1950 kg SS
Titan 4 - 17770 kg LEO (Startkosten 200 - 400 Mio. US-Dollar)
Titan4/Centaur - 4536 kg GEO
Atlas 1 - 2250 kg GTO
Atlas 2 - 2810 kg GTO (Startkosten 75 -85 Mio. US-Dollar)
Atlas 2A - 3045 kg GTO (Startkosten 80 -90 Mio. US-Dollar)
Atlas 2AS - 3668 kg GTO (Startkosten 95 - 105 Mio. US-Dollar)
Atlas 2AR - 3810 kg GTO
X-33 - 15000 kg LEO



NPO Energija

Moskau, Rußland

Sojus U/U2 - 7500 kg LEO



NPO Yuzhnoye

Dnjeprpetrowsk, Ukraine

Zyklon 3/SL-14 - 5500 kg LEO
Zyklon M/SL-11 - 3000 kg LEO
Zenit 2/SL-16 - 1370 kg LEO (Startkosten 35 -45 Mio. US-Dollar)
Zenit 3 - 3280 kg GTO



Nissan Motors, Tokio

Japan
M5 - 2000 kg LEO


Orbital Sciences Corp. (OSC)

Dulles, Virginia, USA

Pegasus - 400 kg LEO
Pegasus XL - 475 kg LEO
Taurus - 1363 kg LEO
X-34 - 550 kg LEO



Rocket Systems Corp.

Tokio, Japan

H2 - 4000 kg GTO (150 - 190 Mio. US-Dollar)
J1 - 870 kg LEO



Abkürzungen:
LEO = Low Earth Orbit (niedrige Erdumlaufbahn)
GEO = Geostationary Orbit (geostationäre Umlaufbahn)
GTO = Geostationary Transfer Orbit (geostationäre Transfer-Umlaufbahn)
SS = Sun Synchronous Orbit (sonnensynchrone Umlaufbahn)


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Copyright 1997 by Motor-Presse Stuttgart. All rights reserved
Last updated November 10, 1997
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