Descriptif

Tutorial group / bureau d’étude « collision risks and mission end of life »

Satellite System Mission & Architecture: example of Kineis – Space IoT provider

Dimensionnement mécanique d’un réservoir spatial (BE de mécanique/matériaux contenant un choix des matériaux)

Project in teams: Set-up as mini project teams (5/6 max). Setup as a red line

• Input: CNES Romain Pinède + Vincent Ruch; Mission requirements; Orbits and constraints (LEO vs GEO)
• Output: final presentation (5mins pitch)

• Process:

  - Step 1: Customer requirements Understand customer requirement; System level engineering (review of system and subsystems for a spacecraft)

  -> Deliverables: requirements & sub-systems overview

  - Step 2: How to organise the project Old Space vs New Space (Telecom satellite vs OneWeb) approach; Project management (PDR, CDR, TRR, FR); Project roles; Quality management (NCR / NRB / lessons learnt)

  -> Deliverable: project charter & project roadmap

  Step 3: System design (ex: mechanism) Redundancy in Space missions; Prime chain vs Redundant chain; FDIR principle; Safety factor; Budgets; Justification approach

  -> Deliverable: Budgets & preliminary design

  Step 4: Final presentation Prepare for PDR (Preliminary Design Review)

  -> Deliverable: Present proposed design of the mechanism + justification approach