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Minotaur I | JAWSAT & FalconSat 1
Orbital Sciences CorporationLaunch Successful

JAWSAT & FalconSat 1

Minotaur I

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Historical mission record

This page records Minotaur I | JAWSAT & FalconSat 1 and its reported outcome: Launch Successful. The date above is a historical record.

Source record updated . This is a source update, not a confirmed launch time.

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Mission status
Launch Successful

Status reported by the mission data provider.

LAUNCH SITEVandenberg SFB, CA, USA

Mission

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.

Launch vehicle
Minotaur I
Mission type
Test Flight
Destination orbit
Low Earth Orbit
Launch pad
Space Launch Complex 8
Provider
Orbital Sciences Corporation

The vehicle

Published configuration and flight history.

Minotaur I
NASA
Launch vehicle

Minotaur I

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
Stages
5
Recorded launches
12
First flight
2000-01-27

Recorded timing

This is a mission record, not an upcoming calendar appointment.

Instantaneous windowPublished target
SCHEDULED MOMENT

A single scheduled moment. The schedule may change before launch.

Launch site & orbit

Vandenberg SFB, CA, USA

The mission in perspective

Launch site & orbit

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Understand this orbit
NASA Blue Marble map of Earth's continents and oceans
Representative orbit · accelerated illustrationNo live tracking or simulated ascent. NASA Blue Marble.

Coverage & sources

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Mission coverage

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Further reading

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