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Antares, Osp-3 user’s guide, Appendix a – payload questionnaire – Orbital Antares User Manual

Page 88

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Antares

®

OSP-3

User’s Guide

Appendix A

– Payload Questionnaire

Release 1.1

July 2013

A-2

SPACECRAFT IDENTIFICATION

FULL NAME:

ACRONYM:

OWNER/OPERATOR:

INTEGRATOR(s):

ORBIT INSERTION REQUIREMENTS*

SPHEROID  Standard

 Other:

ALTITUDE Insertion Apse:

±

 km

±

 nmi

Opposite Apse:

±

 km

±

 nmi

or... Semi-Major Axis:

±

 km

±

 nmi

Eccentricity:

e

INCLINATION

±

deg

ORIENTATION Argument of Perigee:


±

deg

Longitude of Ascending Node (LAN):

±

deg

Right Ascension of Ascending Node (RAAN):


±

deg...for Launch Date:

* Note: Mean orbital elements

LAUNCH WINDOW REQUIREMENTS

NOMINAL LAUNCH DATE:

OTHER CONSTRAINTS (if not already implicit from LAN or RAAN requirements, e.g., solar beta angle, eclipse
time constraints, early on-orbit ops, etc):