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ATHENA WFI Meeting Garching, January 28, 2014 Markus Plattner.

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Presentation on theme: "ATHENA WFI Meeting Garching, January 28, 2014 Markus Plattner."— Presentation transcript:

1 ATHENA WFI Meeting Garching, January 28, 2014 Markus Plattner

2 General ESA Project Lifecycle
General PLM AO: Payload consortium shall be suggested MA: Technology Development shall be finished In B2/C/D Phases dedicated models of ATHENA shall be developed. Type and no. of models depends on model philosophy (BB, EM, QM, FM) ECSS-M-ST-10C_Rev.1(6March2009)_Space project management - Project planning and implementation 11/25/2013

3 Schedule for this Call for L2 Mission Concepts
ATHENA LoI submission deadline: February 2014 (12:00 noon CET) Briefing meeting (ESTEC) 5 March 2014 (tbc) Proposal submission deadline: April 2014 (12:00 noon CET) Proposal evaluation April June 2014 11/25/2013

4 Mission Concept – Expected Content
The mission Concept must address the science goals Top level requirements: High throughput optics: ≈ 2 m² collecting area) High angular resolution: 5 arcsec Wide field of view in the focal plane Energy resolution: 2.5 eV Technical Budget Envelopes: Ariane 5 ECA: < 10 tons mass, 5.4 m diameter, 17 m height < 75 Mbit/s downlink data rate (for Ka band, LagrangePoint L2) Contribution from international partners (upon inter-agency agreements) is limited to 20% of the total mission envelope. 11/25/2013

5 Call for Mission Concept – Important Points
ESA assessment of mission concept: Feasibility, technology readiness, international collaboration scheme (if applicable) Announcement of Opportunity (early 2015 tbc): Consortium shall be selected. Teams or payload consortia shall not be pre-selected in the mission concept The minimum request is to reach TRL 5/6 at mission adoption (2018/2019): Component and/or Breadboard Critical Function Verification in Relevant Environment  Effective overall time for mission preparation including necessary technology developments: 2014 until 2019. Critical Function: Mandatory function which requires specific technology verification When TRL 5 is reached, the element feasibility can be considered as demonstrated, subject to scaling effects. 11/25/2013

6 ATHENA Phase 0 and A Schedule
11/25/2013

7 Work Breakdown Structure – Overview
11/25/2013

8 WFI – Flight Hardware Architecture (1st Draft)
11/25/2013

9 WBS Flight System 11/25/2013

10 WBS Ground Support / Integration & Operation
11/25/2013

11 Work Breakdown Structure – Top Level
11/25/2013


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