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NPSAT-1 Small Satellite

Naval Postgraduate School NPSAT1 Spacecraft

NPSAT1 Mission Information NPSAT-1 CAD Render

The NPSAT1 mission is a small satellite project manifested for launch aboard a Falcon Heavy launch vehicle as part of the Department of Defense (DOD) Space Test Program’s STP-2 mission.  The small, 86 kg (190 lbs), satellite will carry a number of space flight experiments to investigate space weather and the flight demonstration of space technology.  The experiments on-board include the following.

  • Coherent Electromagnetic Radio Tomography Experiment, CERTO (NRL)
  • Langmuir probe (NRL)
  • Configurable, Fault-Tolerant Processor, CFTP (NPS)
  • Solar Cell Measurement System (NPS)
  • Demonstration of Commercial, Off-The-Shelf (COTS) Technology for Space Applications (NPS)

Two experiments are provided by the Naval Research Laboratory (NRL) to measure electron cloud densities in the ionosphere through radio wave propagation from the spacecraft to the earth;  as well as in-situ measurements of ions near the spacecraft.
Spacecraft technology will be flown to demonstrate configurable, fault-tolerant computer technology that can survive and operate in the harsh radiation environment of space.  Computing architectures will be tested to investigate means of correcting errors caused by radiation.  Modifications can be uploaded from the ground to test different configurations of fault tolerance.
Experimental solar cells will be flown along with a solar cell measurement system that will measure the performance of solar cells throughout the 18-month mission life, recording voltage, current, temperatures and solar incidence angles.
Commercial, off-the-shelf (COTS) technology experiments will demonstrate the suitability of commercial sensors and electronics for low-cost solutions to spacecraft technology demands.  Commercial technology such as memory devices, rate sensors and a low-cost digital camera will be flown and operated in space.
Once in orbit, the NPSAT1 spacecraft will provide a platform for experimentation for NPS Space Systems students as a space-based laboratory.  The spacecraft will continue to support graduate education and research, adding to the more than forty Master of Science graduates who have been involved with the project.
NPSAT1 will perform an uncontrolled atmospheric reentry at the end of its mission life.  An autonomous de-orbit module with its own timer will initiate a drag device to bring the spacecraft down to earth.  Analysis has shown that the spacecraft will break up upon reentry, and any debris that might survive would present a negligible risk upon impact.

NPS Key Personnel

  • Principal Investigator:  Dr. Rudolf Panholzer, Chair, Space Systems Academic Group
  • Lead Engineer:  Mr. Daniel Sakoda
  • Electrical Power:  Mr. Ronald Phelps
  • Digital and RF Systems:  Mr. David Rigmaiden
  • Software and Ground Systems:  Mr. James Horning

NPSAT1 Mission Objectives:

  1. Provide a "vehicle" for graduate education in Space Systems Engineering and Space Systems Operations
  2. Provide a platform for space weather experimentation in ionospheric physics
  3. Provide a platform for spacecraft technology demonstration

Program Information:

    Customers: NPS Space Systems Officer Students
    Naval Research Laboratory
  Spacecraft Builder:

Naval Postgraduate School
Space Systems Academic Group

  Launch: Falcon Heavy from Cape Canaveral, FL
    Integrated and flown by the DoD Space Test Program
  Orbit: 720 km circular @ 24° inclination
  Mission Duration: 18 months