Orbital Minotaur VI User Manual
Page 7
Minotaur IV • V • VI User’s Guide
Table of Contents
PAGE
5.3.2.
Payload Interface Circuitry ...................................................................................................... 60
5.3.3.
Payload Battery Charging ........................................................................................................ 60
5.3.4.
Payload Command and Control .............................................................................................. 61
5.3.5.
Pyrotechnic Initiation Signals ................................................................................................... 61
5.3.6.
Payload Telemetry ................................................................................................................... 61
5.3.7.
Payload Separation Monitor Loopbacks .................................................................................. 61
5.3.8.
Telemetry Interfaces ................................................................................................................ 61
5.3.9.
Non-Standard Electrical Interfaces .......................................................................................... 62
5.3.10.
Electrical Launch Support Equipment ................................................................................... 62
5.4.
Payload Design Constraints........................................................................................................ 62
5.4.1.
Payload Center of Mass Constraints ....................................................................................... 62
5.4.2.
Final Mass Properties Accuracy .............................................................................................. 62
5.4.3.
Pre-Launch Electrical Constraints ........................................................................................... 62
5.4.4.
Payload EMI/EMC Constraints ................................................................................................ 62
5.4.5.
Payload Dynamic Frequencies ................................................................................................ 63
5.4.6.
Payload Propellant Slosh ........................................................................................................ 63
5.4.7.
Payload-Supplied Separation Systems ................................................................................... 63
5.4.8.
System Safety Constraints ...................................................................................................... 63
6.
MISSION INTEGRATION .................................................................................................................. 64
6.1.
Mission Management Approach ................................................................................................. 64
6.1.1.
SD/SDL Mission Responsibilities ............................................................................................ 64
6.1.2.
Orbital Mission Responsibilities ............................................................................................... 64
6.2.
Mission Planning and Development ........................................................................................... 65
6.2.1.
Mission Assurance .................................................................................................................. 67
6.3.
Mission Integration Process ........................................................................................................ 68
6.3.1.
Integration Meetings ................................................................................................................ 68
6.3.2.
Mission Design Reviews (MDR) .............................................................................................. 68
6.3.3.
Readiness Reviews ................................................................................................................. 68
6.4.
Documentation ............................................................................................................................ 69
6.4.1.
Customer-Provided Documentation ........................................................................................ 69
6.4.1.1.
Payload Questionnaire ...................................................................................................... 69
6.4.1.2.
ICD Inputs ......................................................................................................................... 69
6.4.1.3.
Payload Mass Properties .................................................................................................. 69
6.4.1.4.
Payload Finite Element Model .......................................................................................... 69
6.4.1.5.
Payload Thermal Model for Integrated Thermal Analysis ................................................. 70
6.4.1.6.
Payload Drawings ............................................................................................................. 70
6.4.1.7.
Program Requirements Document (PRD) Mission Specific Annex Inputs ....................... 70
Release 2.0
June 2013
vi