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Glavni meni

ISO 27852:2016

Space systems — Estimation of orbit lifetime
4. 7. 2016.
95.99   Povučen   23. 2. 2024.

Опште информације

95.99     23. 2. 2024.

ISO

ISO/TC 20/SC 14

Međunarodni standard

49.140  

engleski  

Kupovina

Povučen

Jezik na kome želite da primite dokument.

Apstrakt

ISO 27852:2016 describes a process for the estimation of orbit lifetime for spacecraft, launch vehicles, upper stages and associated debris in LEO-crossing orbits.
It also clarifies the following:
a) modelling approaches and resources for solar and geomagnetic activity modelling;
b) resources for atmosphere model selection;
c) approaches for spacecraft ballistic coefficient estimation.

Životni ciklus

PRETHODNO

POVUČEN
ISO 27852:2011

TRENUTNO

POVUČEN
ISO 27852:2016
95.99 Povučen
23. 2. 2024.

REVIDIRAN OD

OBJAVLJEN
ISO 27852:2024