Orbital Minotaur I - Manual (Page 92)

Minotaur I 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 3.0 March 2014 A-6