{"id":408214,"date":"2024-10-20T05:29:34","date_gmt":"2024-10-20T05:29:34","guid":{"rendered":"https:\/\/pdfstandards.shop\/product\/uncategorized\/bs-iso-233122022\/"},"modified":"2024-10-26T09:59:11","modified_gmt":"2024-10-26T09:59:11","slug":"bs-iso-233122022","status":"publish","type":"product","link":"https:\/\/pdfstandards.shop\/product\/publishers\/bsi\/bs-iso-233122022\/","title":{"rendered":"BS ISO 23312:2022"},"content":{"rendered":"
PDF Pages<\/th>\n | PDF Title<\/th>\n<\/tr>\n | ||||||
---|---|---|---|---|---|---|---|
2<\/td>\n | National foreword <\/td>\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 5 Avoiding release of space debris into Earth orbit during normal operations <\/td>\n<\/tr>\n | ||||||
11<\/td>\n | 6 Avoiding break-ups in Earth orbit 6.1 General 6.2 Accidental break-up caused by an on-board source of energy 6.2.1 General measures <\/td>\n<\/tr>\n | ||||||
12<\/td>\n | 6.2.2 Subsystem-specific measures <\/td>\n<\/tr>\n | ||||||
13<\/td>\n | 6.3 Accidental break-up caused by a collision 6.3.1 Collision avoidance <\/td>\n<\/tr>\n | ||||||
14<\/td>\n | 6.3.2 Assessment of the probability of structural break-up caused by impacts with debris or meteoroid 7 Disposal of spacecraft after the end of mission 7.1 General 7.2 Ensuring execution of disposal action <\/td>\n<\/tr>\n | ||||||
15<\/td>\n | 7.3 Disposal to minimize interference with the GEO protected region 7.3.1 General 7.3.2 Developing basic manoeuvre requirements for a stable disposal orbit 7.3.3 Developing long-term (100-year) disposal orbit characteristics <\/td>\n<\/tr>\n | ||||||
16<\/td>\n | 7.3.4 Determining the manoeuvre sequence 7.4 Disposal to minimize interference with the LEO protected region 7.4.1 General 7.4.2 Re-entry <\/td>\n<\/tr>\n | ||||||
17<\/td>\n | 8 Estimating mass of remaining usable propellant 8.1 General 8.2 Uncertainty of estimation 8.3 Incorporating required function into spacecraft design <\/td>\n<\/tr>\n | ||||||
18<\/td>\n | 8.4 Documentation of data 9 Space debris mitigation plan 9.1 General <\/td>\n<\/tr>\n | ||||||
19<\/td>\n | 9.2 Break-up prevention plan 9.3 End of mission disposal plan (EOMDP) <\/td>\n<\/tr>\n | ||||||
20<\/td>\n | 9.4 Contingency plan <\/td>\n<\/tr>\n | ||||||
21<\/td>\n | Annex A (informative) Procedure for estimating probability of accidental break-up <\/td>\n<\/tr>\n | ||||||
24<\/td>\n | Annex B (informative) Examples of estimation methods <\/td>\n<\/tr>\n | ||||||
27<\/td>\n | Annex C (informative) Deployable drag enhancement device <\/td>\n<\/tr>\n | ||||||
28<\/td>\n | Bibliography <\/td>\n<\/tr>\n<\/table>\n","protected":false},"excerpt":{"rendered":" Space systems. Detailed space debris mitigation requirements for spacecraft<\/b><\/p>\n |