Orbital Minotaur I - Manual (Page 93)

Minotaur I User’s Guide Appendix A
SPACECRAFT SLOSH MODEL*
SLOSH MODEL
UNDER 0 g Pendulum Mass:  lb
m
 kg
Pendulum Length:  ft  m
Pendulum Xs:  in  cm
Attachment Ys:  in  cm
Point Zs:  in  cm
Natural Frequency of Fundamental Sloshing Mode (Hz): ,
SLOSH MODEL
UNDER 1 g Pendulum Mass:  lb
m
 kg
Pendulum Length:  ft  m
Pendulum Xs:  in  cm
Attachment Ys:  in  cm
Point Zs:  in  cm
Natural Frequency of Fundamental Sloshing Mode (Hz): ,
ASCENT TRAJECTORY REQUIREMENTS
Free Molecular Heating at Fairing Separation:
(Standard Service: = 360 Btu/ft
2 /hr)
 Btu/ft 2 /hr
FMH ≤  W/m 2
Fairing Internal Wall Temperature
(Standard Service: = 200°F)  deg F
T ≤  deg C
Dynamic Pressure at Fairing Separation:
(Standard Service: = 0.01 lb
f
/ft 2 )
 lb
f
/ft 2
q ≤  N/m 2
Ambient Pressure at Fairing Separation:
(Standard Service: = 0.3 psia)  lb
f
/in 2
P ≤  N/m 2
Maximum Pressure Decay During Ascent:
(Standard Service: = 0.6 psia)  lb
f
/in 2 /sec
Δ P ≤  N/m 2 /sec
Thermal Maneuvers During Coast Periods:
(Standard Service: none)
Release 3.0 March 2014 A-7