Orbital Antares - Manual (Page 91)

Antares
®
OSP-3
User’s Guide
Appendix A
– Payload Questionnaire
Release 1.1 July 2013 A-5
SPACECRAFT PHYSICAL DIMENSIONS
STOWED
CONFIGURATION Length/Height: in cm
Diameter: in cm
Other Pertinent Dimension(s):
Describe any appendages/antennas/etc which extend beyond the basic satellite envelope:
ON-ORBIT
CONFIGURATION Describe size and shape:
If available, provide electronic files of dimensioned drawings for both stowed and on-orbit configurations.
SPACECRAFT MASS PROPERTIES*
PRE-SEPARATION Inertia units:  lb
m
-in
2
 kg-m
2
Mass:  lb
m
 kg
Ixx: Ixy: XCG:  in  cm
Iyy: Iyy: YCG:  in  cm
Izz: Ixz: ZCG:  in  cm
POST-SEPARATION
(non-separating
adapter remaining with
launch vehicle) Inertia units:  lb
m
-in
2
 kg-m
2
Mass:  lb
m
 kg
Ixx: Ixy: XCG:  in  cm
Iyy: Iyy: YCG:  in  cm
Izz: Ixz: ZCG:  in  cm
* Stowed configuration, spacecraft coordinate frame