Orbital Minotaur VI - Manual (Page 113)

Minotaur IV • V • VI User’s Guide Appendix A
SPACECRAFT MASS PROPERTIES*
PRE-SEPARATION Inertia units:  lb
m
-in
2  kg-m 2
Mass:  lb
m
 kg
Ixx:
Xcg:  in  cm Iyy:
Izz:
Ycg:  in  cm Ixy:
Iyz:
Zcg:  in  cm Ixz:
POST-
SEPARATION
(non-separating
adapter remaining
with launch vehicle)
Inertia units:  lb
m
-in
2  kg-m 2
Mass:  lb
m
 kg
Ixx:
Xcg:  in  cm Iyy:
Izz:
Ycg:  in  cm Ixy:
Iyz:
Zcg:  in  cm Ixz:
* Stowed configuration, spacecraft coordinate frame
Release 2.0 June 2013 A-6