|
Sapphire's primary
mission is to space-qualify micromachined infrared sensors. The
Principal Investigator is Professor Tom Kenny of Stanford
Unviersity. These sensors are part of a JPL program to push the
development of light-weight, inexpensive sensors for spacecraft.
Also on-board are a digital camera and a voice synthesizer.
Sapphire's other mission is to train U.S. Naval Academy midshipmen
in spacecraft operations. For pre-flight integration and
post-launch operations support, SAPPHIRE is managed by Project
Aria at Washington University, St. Louis.
- The structure consists of four
aluminum honeycomb trays, one to a subsystem (from bottom:
Power, Communications, CPU, and Payloads), with eight external
panels (six sides, top and bottom) upon which the solar cells
are mounted. The entire hexagonal cylinder, fully loaded and
on the launch interface, weighs 18 kg (40 lbm).
Sapphire, built by
Stanford University, carries a couple of experiments and a voice
synthesizer microchip designed to convert text messages into a
human voice for transmission over amateur radio frequencies.
There are three payloads and one telemetry
experiment aboard Sapphire: Tunneling Horizon Detectors -
These are a new generation of infrared sensors that detect changes
in IR emission. They are micromachined to fit in a chip and
operate at room temperature. The THDs will see their first flight
aboard Sapphire.
Digital Camera - A Fotoman Plus, a commercially available
black & white camera from Logitech modified for space flight
and planned to photograph North America (around 1km
resolution).
Voice Synthesizer - The Digitalker is to provide a payload
of interest for the Amateur Radio community, specifically in
education.
Telemetry Experiment - A pseudo-payload, designed by
students, is to assess how well we can determine our attitude
using the solar panels as a differential sun sensor.

SAPPHIRE
Stanford
Audiophonic
Photographic
Infrared
Experiment
|
|
SATELLITE
|
| Int'l Designation |
2001 043D
|
Launched
|
| Owner / Sponsor |
NASA/
Stanford / US Naval Academy
|
| Mission |
Technology
|
| Satellite Bus |
Stanford
University
Space Systems Development Laboratory
|
|
| Launch Mass |
18
kg (40 lbm)
|
| Mission Orbit |
500
km (270 nmi)
|
67°
|
| Design Life |
|
| Power (EOL) |
0.016
kW
|
|
LAUNCH
|
| Launch Vehicle
Model |
Athena
1 |
| Launch Date / Time |
2001
Sep 30
|
02:40
|
| Co-Passenger(s) |
Starshine
3
|
| |
PCSat
|
| |
PICOsat
|
|
Financial
|
| Satellite cost |
|
| Web Links |
SAPPHIRE
Website
|
|