Space systems. Best practices for orbit elements at payload. LV separation

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

30-09-2015

Publisher

British Standards Institution

Foreword
Introduction
1 Scope
2 Symbols and abbreviated terms
3 Orbit elements and calculation conditions
4 Calculation method of Keplerian elements
5 Calculation method of orbit elements error
Bibliography

Gives the best practices for orbit elements at payload-LV separation. Covers orbit elements and calculation conditions, calculation method of orbit elements and their errors at elliptical orbit insertion of various payloads.

This Technical Report 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. This Technical Report gives the calculation method of Keplerian elements and the transformation method of all the other orbit elements, in order to satisfy different user’s 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 Technical Report, which can contribute to avoiding possible disputes.

Committee	ACE/68
DocumentType	Standard
Pages	22
PublisherName	British Standards Institution
Status	Current

Standards	Relationship
ISO/TR 19473:2015	Identical

ISO 14303:2002	Space systems — Launch-vehicle-to-spacecraft interfaces
ISO 15863:2003	Space systems Spacecraft-to-launch-vehicle interface control document
NASA CCSDS 504.0-B : ISSUE 1 COR 1 2015	ATTITUDE DATA MESSAGES
NASA CCSDS 502.0-B : ISSUE 2 COR 1 2012	ORBIT DATA MESSAGES
ISO/TR 11233:2014	Space systems Orbit determination and estimation Process for describing techniques
NASA CCSDS 500.0-G : ISSUE 3	NAVIGATION DATA DEFINITIONS AND CONVENTIONS
NASA CCSDS 503.0-B : ISSUE 1 COR 1 2010	TRACKING DATA MESSAGE
AIAA S 131 : 2010(R2016)	ASTRODYNAMICS - PROPAGATION SPECIFICATIONS, TECHNICAL DEFINITIONS, AND RECOMMENDED PRACTICES

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PD ISO/TR 19473:2015

Current

Table of Contents

Abstract

Scope

General Product Information

International Equivalents

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