M00017686
New product
SPACE SYSTEMS - BEST PRACTICES FOR ORBIT ELEMENTS AT PAYLOAD - LV SEPARATION
British Standards Institution
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Availability date: 11/05/2021
Foreword<br>Introduction<br>1 Scope<br>2 Symbols and abbreviated terms<br>3 Orbit elements and calculation conditions<br>4 Calculation method of Keplerian elements<br>5 Calculation method of orbit elements error<br>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.
Published | |
Document Type | Standard |
Status | Current |
Publisher | British Standards Institution |
Pages | |
ISBN | |
Committee | ACE/68 |