User Manual

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):