Minotaur I
Orbital Sciences Corporation
Hersteller
Orbital Sciences Corporation
Familie
Minotaur
Erstflug
2000-01-27
Länge
19.21 m
Durchmesser
1.67 m
Nutzlast LEO
580 kg
Starts
12
Erfolgreich
12
The Minotaur I launch system is derived from converted Minuteman II ICBMs and is used to launch small satellites for the US Government. The first and second stages, taken directly from decommissioned Minuteman missiles, are mated to the Orion third and fourth stages taken from the Pegasus XL air-launched rocket family. An optional hydrazine-powered fifth stage called HAPS can be used.The Minotaur I launch system is derived from converted Minuteman II ICBMs and is used to launch small satellites for the US Government. An optional hydrazine-powered fifth stage called HAPS can be used.


Minotaur ISuccess
NROL-111 · Northrop Grumman Space Systems
Dienstag, 15.06.2021, 13:35 UTC

Minotaur ISuccess
ORS-3 · Orbital Sciences Corporation
Mittwoch, 20.11.2013, 01:15 UTC

Minotaur ISuccess
ORS-1 (USA-231) · Orbital Sciences Corporation
Donnerstag, 30.06.2011, 03:09 UTC

Minotaur ISuccess
NROL-66 (RPP) (USA-225) · Orbital Sciences Corporation
Sonntag, 06.02.2011, 12:26 UTC

Minotaur ISuccess
Tacsat 3 · Orbital Sciences Corporation
Dienstag, 19.05.2009, 23:55 UTC

Minotaur ISuccess
NFIRE · Orbital Sciences Corporation
Dienstag, 24.04.2007, 06:48 UTC

Minotaur ISuccess
Tacsat 2 · Orbital Sciences Corporation
Samstag, 16.12.2006, 12:00 UTC

Minotaur ISuccess
COSMIC 1-6 · Orbital Sciences Corporation
Samstag, 15.04.2006, 01:40 UTC

Minotaur ISuccess
STP-R1 · Orbital Sciences Corporation
Freitag, 23.09.2005, 02:24 UTC

Minotaur ISuccess
XSS-11 · Orbital Sciences Corporation
Montag, 11.04.2005, 13:35 UTC

Minotaur ISuccess
Sindri · Orbital Sciences Corporation
Mittwoch, 19.07.2000, 20:09 UTC

Minotaur ISuccess
JAWSAT & FalconSat 1 · Orbital Sciences Corporation
Donnerstag, 27.01.2000, 03:03 UTC


