{"id":451200,"date":"2024-10-20T09:16:35","date_gmt":"2024-10-20T09:16:35","guid":{"rendered":"https:\/\/pdfstandards.shop\/product\/uncategorized\/bsi-23-30461696-dc\/"},"modified":"2024-10-26T17:17:12","modified_gmt":"2024-10-26T17:17:12","slug":"bsi-23-30461696-dc","status":"publish","type":"product","link":"https:\/\/pdfstandards.shop\/product\/publishers\/bsi\/bsi-23-30461696-dc\/","title":{"rendered":"BSI 23\/30461696 DC"},"content":{"rendered":"
PDF Pages<\/th>\n | PDF Title<\/th>\n<\/tr>\n | ||||||
---|---|---|---|---|---|---|---|
6<\/td>\n | Foreword <\/td>\n<\/tr>\n | ||||||
7<\/td>\n | Introduction <\/td>\n<\/tr>\n | ||||||
9<\/td>\n | 1 Scope 2 Normative references 3 Terms and definitions <\/td>\n<\/tr>\n | ||||||
10<\/td>\n | 4 Symbols (and abbreviated terms) <\/td>\n<\/tr>\n | ||||||
11<\/td>\n | 5 Internal interface requirements 5.1 Unit to unit interface 5.1.1 General 5.1.2 PC-104 Style <\/td>\n<\/tr>\n | ||||||
13<\/td>\n | 5.1.3 Backplane Style <\/td>\n<\/tr>\n | ||||||
14<\/td>\n | 5.2 Mission payload to platform interface 5.2.1 Mechanical connection 5.2.2 Connection methods 5.2.3 Ground lines 5.2.4 Power 5.2.5 Analogue data interface 5.2.6 Digital data interface 5.2.7 Debugging 5.2.8 EMC <\/td>\n<\/tr>\n | ||||||
15<\/td>\n | 5.2.9 Fault isolation and recovery 5.2.10 Harmlessness to other payloads, platform and missions 5.2.11 Safety requirements 5.2.12 Radiation 6 Datasheet requirements for CubeSat units 6.1 General requirements <\/td>\n<\/tr>\n | ||||||
17<\/td>\n | 6.2 Electrical Power System Unit <\/td>\n<\/tr>\n | ||||||
18<\/td>\n | 6.3 Communication Unit 6.4 Command and Data Handling Unit <\/td>\n<\/tr>\n | ||||||
19<\/td>\n | 6.5 Attitude Determination and Control Unit 6.6 Antenna Unit 7 Datasheet requirements for CubeSat platforms 7.1 Mechanical interface <\/td>\n<\/tr>\n | ||||||
20<\/td>\n | 7.2 Electrical Interface 7.3 Software Information 7.4 Operation-related Information 7.5 Safety Information <\/td>\n<\/tr>\n | ||||||
21<\/td>\n | 7.6 Reliability Information 7.7 Assembly, Integration and Testing Information 8 External Electrical Interface (Umbilical) <\/td>\n<\/tr>\n | ||||||
22<\/td>\n | Annex\u20acA (informative) Typical digital data communication for CubeSats <\/td>\n<\/tr>\n | ||||||
24<\/td>\n | Annex\u20acB (informative) PC-104 style example <\/td>\n<\/tr>\n | ||||||
27<\/td>\n | Annex\u20acC (informative) Backplane style example <\/td>\n<\/tr>\n | ||||||
37<\/td>\n | Bibliography <\/td>\n<\/tr>\n<\/table>\n","protected":false},"excerpt":{"rendered":" BS ISO 17981 Space systems \u2014 CubeSat interface<\/b><\/p>\n |