BS ISO 23312:2022
$142.49
Space systems. Detailed space debris mitigation requirements for spacecraft
Published By | Publication Date | Number of Pages |
BSI | 2022 | 30 |
PDF Catalog
PDF Pages | PDF Title |
---|---|
2 | National foreword |
6 | Foreword |
7 | Introduction |
9 | 1 Scope 2 Normative references 3 Terms and definitions |
10 | 4 Symbols and abbreviated terms 5 Avoiding release of space debris into Earth orbit during normal operations |
11 | 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 |
12 | 6.2.2 Subsystem-specific measures |
13 | 6.3 Accidental break-up caused by a collision 6.3.1 Collision avoidance |
14 | 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 |
15 | 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 |
16 | 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 |
17 | 8 Estimating mass of remaining usable propellant 8.1 General 8.2 Uncertainty of estimation 8.3 Incorporating required function into spacecraft design |
18 | 8.4 Documentation of data 9 Space debris mitigation plan 9.1 General |
19 | 9.2 Break-up prevention plan 9.3 End of mission disposal plan (EOMDP) |
20 | 9.4 Contingency plan |
21 | Annex A (informative) Procedure for estimating probability of accidental break-up |
24 | Annex B (informative) Examples of estimation methods |
27 | Annex C (informative) Deployable drag enhancement device |
28 | Bibliography |