Picosatellite System
The Mothership-Daugthership
Mission Architecture
Recently,
a new mission architecture has been suggested to perform distributed sensing
in space. In this architecture, a main satellite, or "mothership",
deploys a number of smaller satellites, or "daughterships", to remote locations
of interest to perform the required sensing. To date, several missions
have placed one or two sensors in interesting locations, but placing dozens
or hundreds of them remains a challenge. Due to increased interest
in distributed sensing in space, new technologies need to be developed.
The mothership technologies include picosatellite storage, deployment,
communication, and retrieval or disposal. The daughtership technologies
include all the necessary miniaturizations of current satellite technology
to meet the picosatellite scale. The primary mission of the OPAL
picosatellite payload is to validate the mothership mission architecture
and provide a basic testbed to develop the mothership and daughtership
technologies.
To the right is an artist's
rendition of the OPAL satellite with a picosatellite being deployed (picture
by Clem Tillier).
The Mothership
The
OPAL design team will focus on mothership technology development.
A picosatellite launcher is under development that addresses the storage
and deployment technologies. The launcher is being designed for scalability,
manufacturability, and reliability. It will be capable of launching
at least three picosatellites. The following pages describe the OPAL
picosatellite launcher:
The Daughtership
The
daughterships are called picosatellites because of their low mass (less
than 1 kg). To satisfy OPAL's end-to-end mission demonstration, the picosatellites
will be capable of communicating data to the ground, either directly or
through a communication system onboard OPAL. The picosatellites will
be built by the following design teams:
During the picosatellite payload
development, several studies and interface documents have been created.
They are listed blow.
-
Technical papers
-
Picosatellite Launch Dynamics
-
Picosatellite Thermal Modeling
-
Picosatellite Interface Document
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Revision
G - Released October 9, 1998 (If the picosatellite drawing does not
print well, here is the gif version.)