SEDSAT-2 Systems:General Specifications, Characteristics and Interface design
From SEDSWiki
Timelines:
- 29 April: Payload Subsystem presents final concepts for payload for team to discuss.
- 06 May: Entire SEDSAT-2 team chooses the payload.
- 13 May: Outline of Payload Selection Study (PSS) due.
- 20 May: First draft of PSS due.
- 27 May: Final draft of PSS due. Payload Selection Review (PSR) begins, reviewed by advisers.
- 03 June: Interface tables due.
Kirk's weight budget: (copied from here)
| Structure | 300g |
| Payload | 200g |
| Attitude Control | 100g |
| Power | 250g |
| Communications | 100g |
| Margin | 50g (can't use this) |
- Total: 1000g
Structure Requirements
Just posted it here. Hopefully you can make it into a matrix where everyone can see. Pradeep 10:32, 13 May 2007 (MDT)Pradeep
- Area (lxb terms) covered by the equipment
- Volume occupied by the equipment
- Mass of the component.
- Heat generated or required
- Optimum Working Temperatures of the component

