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ESA Open Invitation To Tender AO8194
Open Date: 30/01/2015
Closing Date: 11/03/2015

ESA Open Invitation To Tender AO8152
Open Date: 14/11/2014
Closing Date: 22/01/2015

ESA Open Invitation To Tender AO8138
Open Date: 12/11/2014
Closing Date: 21/01/2015

ESA Open Invitation To Tender AO8145
Open Date: 11/11/2014
Closing Date: 09/12/2014

ESA Open Invitation To Tender AO7507
Open Date: 18/04/2013
Closing Date: 30/05/2013

ESA Open Invitation To Tender AO7462
Open Date: 04/04/2013
Closing Date: 30/05/2013



Status: ISSUED
Reference Nr.: 12.1TF.18
Prog. Ref.: ARTES 1-V Budget Ref.: E/0501-01A - ARTES 1-V
Special Prov.: B+DK+F+D+I+NL+E+S+CH+GB+IRL+A+N+FIN+POR+GR+LUX+CZ+CDN+PL+RO
Proc. Prop: NO
Tender Type: C
Price Range: 200-500 KEURO
Establishment: ESTEC
Directorate: Directorate Telecom & Integrated Applica
Department: Telecom Technologies,Product&Systems
Dep Division: Future Projects Division
Contract Officer: Ulrich Sterzl
Last Update Date: 04/04/2013
Update Reason: Tender issue

The aim of the present activity is (1) to synthesise the requirements on DSM based components when used for the next generation of OBP-based payload architectures, (2) to validate the benefits of using the DSM technology for OBP based payloads and (3) to define the associated technological roadmaps.

If you wish to access the documents related to the Invitation to Tender, you have to log in to the ESA portal.

ESA Open Invitation To Tender AO7497
Open Date: 15/04/2013
Closing Date: 27/05/2013



Status: ISSUED
Reference Nr.: 11.1ED.04
Prog. Ref.: TRP
Budget Ref.: E/0901-01 - TRP
Special Prov.: B+DK+F+D+I+NL+E+S+CH+GB+IRL+A+N+FIN+POR+GR+LUX+CZ+RO+PL
Tender Type: C
Price Range: 200-500 KEURO
Establishment: ESTEC
Directorate: Directorate of Technical & Quality Manag
Department: Electrical Engineering Department
Division: Data Systems Division
Contract Officer: Anna Karger-Kocsis
Last Update Date: 15/04/2013
Update Reason: Tender issue

Objectives: This activity will build a configurable Test Bed to validate Failure Detection Isolation and Recovery (FDIR) concepts and implementations for spacecraft Avionics data systems. As an important result of this activity a report containing recommendations and suggestion in advance of an ECSS standard for a correct design and implementation of FDIR concepts (for the part that affects the Avionics Data system). Description: Starting from the already available Reference Architecture System Testbed for Avionics (RASTA) system and pushed by recent anomaly events, the aim is to have a real HW test-bed where the conceived or implemented FDIR concepts can be validated. The currently available RASTA system has to be upgraded mainly in order to: - implement redundancies (needed to test FDIR concepts); - improve its configurability/functionality features. At the same time the opportunity will be taken to take account of the latest processor modules (e.g. LEON 3, SCOC?). The upgrade will also provide the reference platform for all applicable building block activities. Reconfiguration Mechanisms, correct use of Safe Guard Memory, fault coverage, BIT are only some of the topics that the availability of a real Test Bed can allow to investigate and validate.

If you wish to access the documents related to the Invitation to Tender, you have to log in to the ESA portal.

ESA Open Invitation To Tender AO7485
Open Date: 12/04/2013
Closing Date: 24/05/2013



Status: ISSUED
Reference Nr.: 13.138.01
Prog. Ref.: GSTP Period 5 Elem 4
Budget Ref.: E/0904-054 - GSTP Period 5 Elem 4
Special Prov.: CH
Tender Type: C
Price Range: 200-500 KEURO
Establishment: ESTEC
Directorate: Directorate of Technical & Quality Manag
Department: System, Software & Technology Department
Division: Systems and Cost Engineering Division
Contract Officer: Franziska Erkelens-Sickinger
Last Update Date: 23/04/2013
Update Reason: Summary updated

CubeSat nanosatellites may serve to develop, demonstrate and operationally validate some active debris removal technologies at low cost before they are used on larger operational missions to remove defunct spacecraft and upper stages. Critical technologies to be developed include GNC sensors, actuators and software for rendezvous and close proximity operations, debris capture mechanisms, and propulsion or other devices for de-tumbling and de-orbiting. This activity covers the evaluation and trade-off of technologies relevant to Active Debris Removal to be later developed in miniaturised form in a follow-on activity and intended to be finally demonstrated in Low Earth Orbit on a CubeSat nano-satellite mission.

If you wish to access the documents related to the Invitation to Tender, you have to log in to the ESA portal.