Performance capability, margins and reserves, including description of how performance reserve is calculated Sequence of events and tracking coverage Time history of trajectory from launch to targeted condition and end of mission maneuvers Launch vehicle summary weight statement Sources and magnitude for all dispersions used. If statistical dispersions are used, then the distribution method (e.g., normal, gaussian) shall be specified for each parameter Definition of all coordinate systems used Reference to the source(s) for all payload and launch vehicle inputs to this analysis (e.g., requirements, mass properties) Evaluation of compliance with applicable ICD requirements and constraints. (K) Launch windows determined by analysis (L) Input file CDRL DESCRIPTION Number: C4-2 FINAL MISSION ANALYSIS (FMA) DESCRIPTION/PURPOSE: This analysis is prepared based on payload requirements resulting from NASA review of the PGAA and contains information similar to that in the PGAA. This analysis supports pre-flight verification of compliance with mission requirements. DATA REQUIREMENTS: The FMA shall include, as a minimum: The nominal 5 or 6 Degree of Freedom (DOF) trajectory simulation for each targeted insertion condition utilizing actual weights and propulsion models (electronic format is preferred). All Data Requirements identified in PGAA Data Requirement Description.
Performance capability, margins and reserves, including description of how performance reserve is calculated Sequence of events and tracking coverage Time history of trajectory from launch to targeted condition and end of mission maneuvers Launch vehicle summary weight statement Sources and magnitude for all dispersions used. If statistical dispersions are used, then the distribution method (e.g., normal, gaussian) shall be specified for each parameter Definition of all coordinate systems used Reference to the source(s) for all payload and launch vehicle inputs to this analysis (e.g., requirements, mass properties) Evaluation of compliance with applicable ICD requirements and constraints. (K) Launch windows determined by analysis (L) Input file CDRL DESCRIPTION Number: C4-2 FINAL MISSION ANALYSIS (FMA) DESCRIPTION/PURPOSE: This analysis is prepared based on payload requirements resulting from NASA review of the PGAA and contains information similar to that in the PGAA. This analysis supports pre-flight verification of compliance with mission requirements. DATA REQUIREMENTS: The FMA shall include, as a minimum: The nominal 5 or 6 Degree of Freedom (DOF) trajectory simulation for each targeted insertion condition utilizing actual weights and propulsion models (electronic format is preferred). All Data Requirements identified in PGAA Data Requirement Description.
146413-SOL-001-003.docx