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On-Orbit
Verification TET
Due
to the high safety standards in the space industry every
new product must go through a verification process before qualifying
for operation in a space system. Within the verification process
the payload undergoes a series of tests which prove that it
is in accordance with mission requirements in terms of function,
reliability and safety.
Important verification components are the qualification for
use on the ground as well as the On-Orbit Verification (OOV),
i.e. proof that the product is suitable for use under virtual
space conditions (on-orbit). Here it is demonstrated that the
product functions under conditions which cannot or can only
be partially simulated on the ground.
As
prime contractor for the TET-1 mission the responsibilities
of Kayser-Threde include
- Definition & management
of Ground-, Space- and Launch Segment
- Technical
support of Payload suppliers
- Development
of Payload Segment
- Control
of Satellite Bus development, performed by Astro- und Feinwerk-technik
Adlershof GmbH, Berlin
- Control
of Ground Segment develop-
ment, performed by DLR-GSOC, Oberpfaffenhofen.
11
payloads have been selected by DLR for the first
TET mission. The payloads are developed by 11 different
companies and institutions and comprise newest technology
to be demonstrated for usage in space environment. The
technical areas cover next generation solar arrays, navigation
equipment, batteries, cameras, communication equipment,
and satellite propulsion system and computer hardware.
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The
payload to satellite bus interface is realized and managed by a modular
payload supply system developed by Kayser-Threde, allowing
to be customized with minimum effort to the experiment needs
and thereby reducing the effort for recurring missions.
TET-1
will be launched in a piggy-back configuration into a Low Earth
Orbit with a Soyuz launcher with Fregat upper stage from
Baikonur. The launch is planned for mid 2010, limiting the
development time to about 24 months.
The
project has successfully passed the PDR and is about to start the
detailed design & manufacturing phase. Launch negotiations
have been performed as well as the contracts with the payload
providers have been signed.
TET-1 Technical Data |
| Dimensions |
880 mm x 550 mm x 650 mm (H x W x D) with about 90 liters
of payload compartment |
| Mass |
Bus 70 kg
Payload 50 kg |
| Number of payloads |
11 |
| Stabilization |
3-axes |
| Pointing accuracy |
5 arcmin |
| Payload power consumption |
max. 20 W continuous |
| Uplink rate |
4 kbit/s |
| Downlink rate |
2.2 Mbit/s high rate |
| Orbit |
550 km, SSO |
| Launch |
Mid 2010 |
| Mission duration |
one year |
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