Minotaur I
Orbital Sciences Corporation
Manufacturer
Orbital Sciences Corporation
Family
Minotaur
Maiden flight
2000-01-27
Length
19.21 m
Diameter
1.67 m
Payload to LEO
580 kg
Launches
12
Successful
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
Tuesday, Jun 15, 2021, 13:35 UTC

Minotaur ISuccess
ORS-3 · Orbital Sciences Corporation
Wednesday, Nov 20, 2013, 01:15 UTC

Minotaur ISuccess
ORS-1 (USA-231) · Orbital Sciences Corporation
Thursday, Jun 30, 2011, 03:09 UTC

Minotaur ISuccess
NROL-66 (RPP) (USA-225) · Orbital Sciences Corporation
Sunday, Feb 6, 2011, 12:26 UTC

Minotaur ISuccess
Tacsat 3 · Orbital Sciences Corporation
Tuesday, May 19, 2009, 23:55 UTC

Minotaur ISuccess
NFIRE · Orbital Sciences Corporation
Tuesday, Apr 24, 2007, 06:48 UTC

Minotaur ISuccess
Tacsat 2 · Orbital Sciences Corporation
Saturday, Dec 16, 2006, 12:00 UTC

Minotaur ISuccess
COSMIC 1-6 · Orbital Sciences Corporation
Saturday, Apr 15, 2006, 01:40 UTC

Minotaur ISuccess
STP-R1 · Orbital Sciences Corporation
Friday, Sep 23, 2005, 02:24 UTC

Minotaur ISuccess
XSS-11 · Orbital Sciences Corporation
Monday, Apr 11, 2005, 13:35 UTC

Minotaur ISuccess
Sindri · Orbital Sciences Corporation
Wednesday, Jul 19, 2000, 20:09 UTC

Minotaur ISuccess
JAWSAT & FalconSat 1 · Orbital Sciences Corporation
Thursday, Jan 27, 2000, 03:03 UTC


