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Launch Vehicle Production and Operations Cost Metrics
Author(s) -
Mick Watson,
James R. Neeley,
Ruby F. Blackburn
Publication year - 2014
Publication title -
2018 spaceops conference
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2014-1606
Subject(s) - variable cost , cost driver , metric (unit) , payload (computing) , computer science , geostationary orbit , cost estimate , unit cost , variable (mathematics) , production (economics) , operations research , reliability engineering , engineering , operations management , systems engineering , aerospace engineering , satellite , mathematics , business , economics , macroeconomics , mechanical engineering , computer network , mathematical analysis , accounting , marketing , network packet
Traditionally, launch vehicle cost has been evaluated based on $/Kg to orbit. This metric is calculated based on assumptions not typically met by a specific mission. These assumptions include the specified orbit whether Low Earth Orbit (LEO), Geostationary Earth Orbit (GEO), or both. The metric also assumes the payload utilizes the full lift mass of the launch vehicle, which is rarely true even with secondary payloads.1,2,3 Other approaches for cost metrics have been evaluated including unit cost of the launch vehicle and an approach to consider the full program production and operations costs.4 Unit cost considers the variable cost of the vehicle and the definition of variable costs are discussed. The full program production and operation costs include both the variable costs and the manufacturing base. This metric also distinguishes operations costs from production costs, including pre-flight operational testing. Operations costs also consider the costs of flight operations, including control center operation and maintenance. Each of these 3 cost metrics show different sensitivities to various aspects of launch vehicle cost drivers. The comparison of these metrics provides the strengths and weaknesses of each yielding an assessment useful for cost metric selection for launch vehicle programs.

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