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Minotaur · Orbital ATK

Minotaur I

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Specifications

Status
active
Height
19.21 m
Diameter
1.67 m
Mass
36,000 kg
Stages
5
Payload to LEO
580 kg
First flight
2000-01-27
Total launches
12
Success / Fail
12 / 0

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.

Payloads it launched · 62

USA 317
LEO
USA 316
LEO
USA 318
LEO
BLACK KNIGHT
LEO
COPPER
LEO
ORS TECH 2
LEO
PROMETHEUS 1-6
LEO
FIREFLY
LEO
PROMETHEUS 1-5
LEO
PROMETHEUS 1-3
LEO
SENSE SV1
LEO
STPSAT-3
LEO
SENSE SV2
LEO
ORS TECH 1
LEO
HORUS
LEO
PHONESAT 2.4
LEO
DRAGONSAT
LEO
PROMETHEUS 1-2
LEO
ORSES
LEO
PROMETHEUS 1-7
LEO
NPS-SCAT
LEO
CAPE-2
LEO
CHARGERSAT
LEO
VERMONT LUNAR
LEO