|
SNAP-1’s
primary payload is a machine vision system (MVS) which will enable
the inspection of other spacecraft in orbit. The MVS consists of
three ultra-miniature wide-angle CMOS video cameras and one
narrow-angle CMOS video camera, together with sophisticated image
processing electronics. The MVS will also be used to provide
medium resolution images of the Earth from SNAP-1’s 650km
altitude, near-polar orbit. The near infra-red filter in the
narrow angle camera provides good discrimination between land, sea
and clouds and allows the camera to produce clear images through
the otherwise hazy atmosphere at 500m ground resolution. Using its
miniature propulsion, navigation and inter-satellite link systems,
SNAP-1 will attempt to rendezvous in orbit with its companion
spacecraft, Tsinghua-1. SNAP-1 was designed and built by SSTL with
its own funds in under one year and at an overall mission cost,
including development, launch and commissioning, of less then
US$1.5 million.
SNAP
1
Surrey
Nanosatellite
Applications
Platform
|
|
Satellite
|
| Int'l Designation |
2000
033B
|
launched
|
| Owner / Sponsor |
Surrey
Satellite Technology Ltd. (SSTL)
|
| Mission |
Demonstrator
|
| Constellation/Block |
|
| Launch Mass |
6.5
kg (14 lbm)
|
| Dimensions, stowed |
|
| Mission Orbit |
SSO /
650 km (400 miles) circular
|
|
| Design Life |
|
| Power (EOL) |
|
|
Launch
|
| Launch Vehicle
Model |
Kosmos
3M |
| Co-passenger(s) |
Nadezhda
6/COSPAS |
| |
Tsinghua
1 |
| Date / Time (UTC) |
2000
Jun 28
|
10:37
|
|
Financial
|
| Satellite cost |
US$1.5
million
|
| Web Links |
|
|