Watch the Launch

ORS-1 (USA-231)

Overview

Destination: Low Earth Orbit
Mission: Government/Top Secret

Low Earth Orbit Launch Area 0 B Wallops Flight Facility, Virginia, USA

ORS-1 satellite is designed to provide orbital space imagery of Southwest Asia and to enhance battlespace awareness to operational field commanders.

Minotaur I

Family:
Configuration:

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.

Specifications
  • Minimum Stage
    4
  • Max Stage
    5
  • Length
    19.21 m
  • Diameter
    1.67 m
  • Fairing Diameter
  • Launch Mass
    36.0 T
  • Thrust
    935.0 kN
Family
  • Name
    Minotaur I
  • Family
  • Variant
  • Alias
    Minotaur OSP-SLV
  • Full Name
    Minotaur I
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
    580.0 kg
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity
    331.0 kg

Orbital Sciences Corporation

Orbital Sciences Corporation

(OSC)

Successes: 65 Failures: 7 Pending: 0

Agency Type:

INFO WIKI

Wallops Flight Facility, Virginia, USA

Launch Area 0 B


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