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OSC Minotaur I JAWSAT & FalconSat 1 - space launch mission detailed information

When is OSC Minotaur I JAWSAT & FalconSat 1? Launch date 27/JAN/2000 — Minotaur I rocket launch by Orbital Sciences Corporation from Space Launch Complex 8.

OSC Minotaur I JAWSAT & FalconSat 1 launch date, launch time, live countdown, live stream and mission status (Success) — tracked on Space Realm.

OSC Minotaur I JAWSAT & FalconSat 1

Minotaur I rocket used for the JAWSAT & FalconSat 1 space launch

Minotaur I

USA flag — Minotaur I rocket external-link-icon-img

Status

Success

Date

27 JAN 2000

03:03

Mission Overview

The JAWSAT (Joint Air Force Academy / Weber State University Satellite) project was developed by students working alongside aerospace professionals. Initially designed with a pulsed-plasma thruster to train Air Force Academy cadets (see JAWSAT), the mission has since evolved to include the efforts of several universities, local aerospace companies, the Air Force Academy, the Air Force Research Laboratory, and NASA. Utilizing breakthrough technologies, JAWSAT deployed four satellites when it reached orbit. The onboard imaging system recorded the deployment of each payload with its six digital cameras. The first free-flying Academy satellite, FalconSat-1 carried the CHAWS (Charging Hazards and Wake Studies) experiment developed by the Physics Department at the Academy.

Rocket

Minotaur I

Mission Type

Test Flight

Orbit

Low Earth Orbit

Stages

5

Livestream

Not available

Rocket Details

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.

Height

19.21 m

Diameter

1.67 m

Launch Mass

36 T

Thrust

935 kN

Version: 2.11.2

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