Expected development maturity under contract (spec) should correlate with Project/Program Approved MGA Depletion Schedule in Mass Properties Control Plan. If specification NTE, MGA is inclusive of Actual MGA (A5 & A6). If specification is not an NTE Actual MGA (e.g. nominal), then MGA values are reduced by A5 values and A5 is representative of remaining uncertainty. Basic Mass = Engineering Estimate based on design and construction principles with NO embedded margin MGA Mass = Basic Mass * assessed % from approved MGA schedule. Predicted Mass = Basic + MGA. Aggregate MGA % = (Aggregate Predicted - Aggregate Basic) /Aggregate Basic
Baseline definition and system optimization are used for the analysis of programmed holds developed ...
Mass Estimating Relationships (MERs) have been developed for use in the Program to Optimize Simulate...
The NASA Engineering and Safety Center was requested to improve on the Best Practices document produ...
Current Verbiage in S-120 Applies to Dry Mass. Mass Margin is difference between Required Mass and P...
Mass has been widely used as a variable input parameter for Cost Estimating Relationships (CER) for ...
Abstract In the assessment of system's developmental maturity, metrics are used for making effe...
Computer weight/performance prediction method to assess design and program and to optimize structura...
Overview of the measurement uncertainty process at NASA GRC. Examples drawn from the 8 by 6 SWT anal...
An integrated tool called the Multi Mission System Analysis for Planetary Entry Descent and Landing ...
Weight estimating and forecasting of manned space systems during conceptual design - handboo
Model Based Systems Engineering (MBSE) has recently been gaining significant support as a means to i...
Most space programs experience significant cost and schedule growth over the course of program devel...
Various space electrical power system masses are analyzed with particular emphasis on the power mana...
Part of NASAs In-Space Propulsion Technology (ISPT) program is the development of the tradespace to ...
System analysis and design of any entry system must balance the level fidelity for each discipline a...
Baseline definition and system optimization are used for the analysis of programmed holds developed ...
Mass Estimating Relationships (MERs) have been developed for use in the Program to Optimize Simulate...
The NASA Engineering and Safety Center was requested to improve on the Best Practices document produ...
Current Verbiage in S-120 Applies to Dry Mass. Mass Margin is difference between Required Mass and P...
Mass has been widely used as a variable input parameter for Cost Estimating Relationships (CER) for ...
Abstract In the assessment of system's developmental maturity, metrics are used for making effe...
Computer weight/performance prediction method to assess design and program and to optimize structura...
Overview of the measurement uncertainty process at NASA GRC. Examples drawn from the 8 by 6 SWT anal...
An integrated tool called the Multi Mission System Analysis for Planetary Entry Descent and Landing ...
Weight estimating and forecasting of manned space systems during conceptual design - handboo
Model Based Systems Engineering (MBSE) has recently been gaining significant support as a means to i...
Most space programs experience significant cost and schedule growth over the course of program devel...
Various space electrical power system masses are analyzed with particular emphasis on the power mana...
Part of NASAs In-Space Propulsion Technology (ISPT) program is the development of the tradespace to ...
System analysis and design of any entry system must balance the level fidelity for each discipline a...
Baseline definition and system optimization are used for the analysis of programmed holds developed ...
Mass Estimating Relationships (MERs) have been developed for use in the Program to Optimize Simulate...
The NASA Engineering and Safety Center was requested to improve on the Best Practices document produ...