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[1]- © TU Berlin
BEESAT-2 [2]
The primary scientific objective of the
mission is the technical verification of an innovative attitude
control system for picosatellites under space conditions.
more to: BEESAT-2
[3]
BEESAT-4 [4]
BEESAT-4 is the most recent mission of the
BEESAT-series. The main objective is the implementation of a precise
positioning and orbit determination package and its on orbit
verification.
more to: BEESAT-4
[5]
DECAN [6]
The DECAN project allows aerospace engineering
students at the TU Berlin to develop, manufacture, test and launch a
two-stage sounding rocket.
more to: DECAN
[7]
FDA [8]
This project deals with laboratory investigations
for a future attitude control system for nano- and pico satellites.
more to: FDA
[9]
Erasmus Mundus MANECA [10]
In the frame of the project,
more than 100 students at all academic levels, academic and
administrative staff from Central Asian universities have received
scholarships for study, research and training at one of the European
partner universities.
more to: Erasmus Mundus
MANECA [11]
iBOSS-2 [12]
The project aims at the development of a
concept for modular satellites enabling autonomous maintenance and
servicing using robotic systems.
more to: iBOSS-2
[13]
MKI [14]
This project deals with the research and
development of satellite components for CubeSats. Combining satellite
components to form compact modules shall increase the possible payload
capacities of pico-satellites.
more to: MKI
[15]
PiNaSys [16]
The PiNaSys project encompasses the
development, manufacturing and demonstration of miniaturized
components for distributed pico- and nanosatellite systems.
more to: PiNaSys
[17]
PROMENG (EU) [18]
The project envisages to improve Master
programmes of Electrical Engineering aligning them with modern
societal conditions of the target partner countries RU, UA and UZ.
more to: PROMENG (EU)
[19]
SEAR [20]
SEAR incorporates developing an autonomous land
vehicle that shall be able to handle a difficult course that resembles
an exploration scenario on a Martian surface. The long term goal is
the development of a space suitable rover for use on an Earth-near
planet.
more to: SEAR
[21]
SALSAT [22]
The objective of the SALSAT mission is to
investigate the global RF spectrum in the VHF, UHF and S-Band using a
novel payload for spectrum analysis in orbit. The nanosatellite SALSAT
will be equipped with the payload as well as launched and operated
within the scope of the project. In addtion, SALSAT features secondary
payloads for the high-precision orbit determination, earth observation
and fluid dynamic actuation for attitude control.
more to: SALSAT
[23]
S-NET [24]
The objective of the S-Net mission is to
investigate and demonstrate the inter-satellite communication
technology within a distributed an autonomously operating
nanosatellite network.
more to: S-NET
[25]
TechnoSat [26]
The TechnoSat nanosatellite mission has
the primary objective to demonstrate and test novel nanosatellite
technologies and components in low earth orbit.
more to: TechnoSat
[27]
TUBIN [28]
TUBIN is a university satellite mission with
the objective to demonstrate novel earth remote sensing technologies
for nanosatellites.
more to: TUBIN
[29]
Head of the Chair
Prof. Dr.-Ing. Enrico Stoll
Phone: +49 30 314-21339
Room F 515
office@space.tu-berlin.de [30]
Contact
Bettina Taube
Room F 516
Marchstraße 12-14
D-10587 Berlin
Phone: +49 (0)30 314-21305
Fax: +49 (0)30 314-21306
------ Links: ------
[1]
http://www.raumfahrttechnik.tu-berlin.de/fileadmin/
fg169/pics/AktuelleProjekte.jpg
[2]
https://www.raumfahrttechnik.tu-berlin.de/menue/res
earch/current_projects/beesat_2/parameter/en/font1/maxh
ilfe/
[3]
https://www.raumfahrttechnik.tu-berlin.de/menue/res
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ilfe/
[4]
https://www.raumfahrttechnik.tu-berlin.de/menue/res
earch/current_projects/beesat_4/parameter/en/font1/maxh
ilfe/
[5]
https://www.raumfahrttechnik.tu-berlin.de/menue/res
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ilfe/
[6]
https://www.raumfahrttechnik.tu-berlin.de/menue/res
earch/current_projects/decan/parameter/en/font1/maxhilf
e/
[7]
https://www.raumfahrttechnik.tu-berlin.de/menue/res
earch/current_projects/decan/parameter/en/font1/maxhilf
e/
[8]
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earch/current_projects/fda/parameter/en/font1/maxhilfe/
[9]
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earch/current_projects/fda/parameter/en/font1/maxhilfe/
[10]
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lfe/
[11]
https://www.raumfahrttechnik.tu-berlin.de/menue/re
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lfe/
[12]
https://www.raumfahrttechnik.tu-berlin.de/menue/re
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e/
[13]
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[14]
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/
[15]
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[16]
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e/
[17]
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e/
[18]
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ilfe/
[19]
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ilfe/
[20]
https://www.raumfahrttechnik.tu-berlin.de/menue/re
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e/
[21]
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[22]
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lfe/
[23]
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lfe/
[24]
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fe/
[25]
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[26]
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xhilfe/
[27]
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xhilfe/
[28]
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[29]
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[30]
https://www.tu-berlin.de/allgemeine_seiten/contact
/parameter/en/font1/maxhilfe/id/54492/?no_cache=1&a
sk_mail=YHOI2QANLumUt3k2WCfTaAcAWIzOILZzRprhATMWM86Afiw
%2BYmaZ9A%3D%3D&ask_name=Prof.%20Dr.-Ing.%20Enrico%
20Stoll