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Composition of eXTP mission

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Presentation on theme: "Composition of eXTP mission"— Presentation transcript:

1 Suggestions and questions on the Management structure of the eXTP Consortium

2 Composition of eXTP mission

3 Management at the Mission Level
Steering Committee Officials from CNSA, CAS, ESA, Space Agencies, CASC office at CNSA Science Advisory Committee Top Scientists in this field, led by PI Secretary at IHEP Science Working Group Leading scientists of the institutions involved, led by PI Scientific simulation, white papers; Simulation and optimization of the payloads; observational strategies and planning Overall mission management office Led by the general manager and chief designer of the mission Schedule, quality & reliability, coordination Office at CASC

4 Management at the Satellite Level
Satellite manager office Manager and his/her assistants (Budget, schedule, quality, coordination) Chief designer and his/her group (Technology, reliability, production, experiments) Design and optimization of the satellite Supervise the design and production of payloads (LAD and WFM via the contact persons at IHEP) Interface between the sub-systems AIT at the sallite level office at CAST

5 Management at the payload Level
Payload manager office Manager and his/her assistants (Budget, schedule, quality, coordination) Chief designer and his/her group (Technology, reliability, production, experiments) Design and optimization of the payloads Supervision of LAD and WFM (schedule, performance, reliability) through the contact persons at IHEP Interface within and between the SFA, PFA, LAD, WFM The instrument groups are responsible for calibration office at IHEP

6 Phases of satellite engineering
Development of the satellite Pre-study Background model study Desgin phase Preflight model phase Flight model phase In-orbit tests In-orbit operation Electric model Structure and thermal model Qualification model

7 Quality Control The developments of SFA and PFA will follow the specifications of CAST, where LAD and WFM (including the devices made in China) will follow the ESA specifications. Platform components will follow the CAST specifications. The conditions of all the environment tests will be given by CAST.

8 Quality Control The three 5-principles ensuring the success of China’s aerospace in the past 3 decades

9 The 5 principles to fix the technical problems:
Locate Accurately Clarify the Mechanism Make the Problem reappear Effective Measures Ensure no similar problems exist A report on each problem is needed to address in the above 5 aspects. LAD and WFM will follow the ESA regulations, but need to report to the payload chief designer.

10 The 5 principles to manage the change of the technical conditions:
Sufficient demonstration Agreement from every side Experimental verification Complete approval Real implementation A review report on each change is needed to address from the above 5 aspects. LAD and WFM need to follow the same regulations if it changes the IDS with the platform.

11 Management of the development of SGS
SGS manager office Manager and his/her assistants (Budget, schedule, coordination) Chief designer and his/her group (Requirements, design, tests) office at IHEP

12 Schedule control A first-level CPM programme will be created by the mission manager office, and then CPM programme at a lower level. Regular meeting every two weeks between the satellite manager office and the payload manager office, and video meeting every two weeks between the payload manager office and the leaders of the 4 instrument teams. One dispatcher for each instrument group, the IHEP contact persons for LAD and WFM act as the dispatchers for these two teams in the regular meetings. Annual meeting for the whole project to review the progress made in the past year, and to schedule the important events in the coming year.

13 Documents The IDS should be in English.
The overall design reports of LAD and WFM should have Chinese version, and the two contact persons are responsible for the translation of the two reports. (??) For other issues, the CAS-ESA SMILE satellite and the China-Brasil Earth-Resource satellite can be taken as references. Should the overall design report of the satellite also have an English version, as long as the confidential sections are eliminated?


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