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NRO L-111 Launch

UPDATE: We're holding the count due to storms in the area and will delay the start of the live stream. Stay tuned for updates! A Northrop Grumman Corporation #Minotaur rocket carrying three national ...

Minotaur NROL111

NROL-111 Mission UpdateSet to launch | June 15, 2021 between 6:30-11:30 a.m. EDTWatch live on NASA Wallops YouTube channel.Follow our social media accounts:&nbs

NROL-111

Circle Image

Overview

Destination: Low Earth Orbit
Mission: Government/Top Secret

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

Classified payload for the U.S. National Reconnaissance Office.

Updates

Nosu • June 15, 2021, 4:02 p.m.

Launch success confirmed by the US Space Force's Space and Missile Systems Center


Nosu • June 15, 2021, 11:09 a.m.

Now targeting 13:35 UTC


Nosu • June 15, 2021, 8:37 a.m.

Hold at T-minus 2 hours 30 minutes


Nosu • June 8, 2021, 5:41 p.m.

Targeting 11:00 UTC


Nosu • June 1, 2021, 6:20 p.m.

Launch window confirmed. Setting GO.


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
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