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ISO/TR 19473:2015
Space systems — Best practices for orbit elements at payload — LV separation
Automaticky preložený názov:
Vesmírne systémy - osvedčené postupy pre orbitálnych prvkov pri užitočného zaťaženia - separačné LV
NORMA vydaná dňa 2.9.2015
Informácie o norme:
Označenie normy: ISO/TR 19473:2015
Dátum vydania normy: 2.9.2015
Kód tovaru: NS-615153
Počet strán: 12
Približná hmotnosť: 36 g (0.08 libier)
Krajina: Medzinárodná technická norma
Kategória: Technické normy ISO
Kategórie - podobné normy:
Anotácia textu normy ISO/TR 19473:2015 :
Description / Abstract: ISO/TR 19473:2015 provides the best practices for orbit elements at payload-LV separation. It includes orbit elements and calculation conditions, calculation method of orbit elements and their errors at elliptical orbit insertion of various payloads. The fit between the actual and expected values of orbit elements can be used as a criterion of commercial launch. There are many different sets of orbit elements. Each is best suited for a particular application. The traditionally used set of orbital elements is called the set of Keplerian elements. ISO/TR 19473:2015 gives the calculation method of Keplerian elements and the transformation method of all the other orbit elements, in order to satisfy different users need. Affected by terrestrial gravitational perturbation, lunisolar gravitation perturbation and other factors, orbit elements change slowly after orbit injection. Orbit elements calculation methods after separation are not included in this Technical Report. The technical communication and specific progress for orbit elements is relatively easy to be agreed on by applying this ISO/TR 19473:2015, which can contribute to avoiding possible disputes.
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