Orbital Minotaur I - Manual (Page 94)

Minotaur I User’s Guide Appendix A
SPACECRAFT ENVIRONMENTS
THERMAL
DISSIPATION Spacecraft Thermal Dissipation, Pre-Launch Encapsulated: Watts
Approximate Location of Heat Source:
Thermal Control Provisions: (Paint, Tape, etc.):
TEMPERATURE Temperature Limits During Max  deg F  deg C
Ground/Launch Operations: Min  deg F  deg C
(Standard Service is 55°F to 80°F)
Component(s) Driving Temperature Constraint:
Approximate Location(s):
HUMIDITY Relative Humidity: or, Dew Point:
Max % Max  deg F  deg C
Min % Min  deg F  deg C
(Standard Service is 37 deg F)
NITROGEN
PURGE Specify Any Nitrogen Purge Requirements, Including Component Description,
Location, and Required Flow Rate:
(Nitrogen Purge is a Non-Standard Service)
CLEANLINESS Volumetric Requirements (e.g. Class 100,000):
Surface Cleanliness (e.g. Visually Clean):
Other:
LOAD LIMITS Ground Transportation Load Limits Axial ≤ g’s Lateral ≤ g’s
Release 3.0 March 2014 A-8