Satellite servicing mission preliminary cost estimation model
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Satellite servicing mission preliminary cost estimation model

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Published by National Aeronautics and Space Administration in [Washington, DC? .
Written in English


  • Astronautics.

Book details:

Edition Notes

Statementprepared by Advanced Planning and Analysis Division, Space Sciences Department, Science Applications International Corporation.
SeriesNASA-CR -- 171978., [SAIC report] -- rept. no. SAIC 87/1514., NASA contractor report -- NASA CR-171978., SAIC report -- no. SAIC 87/1514.
ContributionsUnited States. National Aeronautics and Space Administration.
The Physical Object
Pagination1 v.
ID Numbers
Open LibraryOL15275995M

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Point estimate generated by any cost model does not reflect uncertainty or risk • Two sources of error: general cost estimating uncertainty and technical risk –General cost estimating uncertainty is an attribute of the model •In SSCM, it is quantified by the SEE –Technical risk is an attribute of the mission under development. Space Infrastructure Servicing (SIS) is a spacecraft being developed by Canadian aerospace firm MacDonald, Dettwiler and Associates to operate as a small-scale in-space refueling depot for communication satellites in geosynchronous orbit.. In June , SSL announced its first commercial customer, Luxembourg-based satellite owner/operator SES S.A. brings you the latest images, videos and news from America's space agency. Get the latest updates on NASA missions, watch NASA TV live, and learn about our quest to reveal the unknown and benefit all by: 1. Project Cost Breakdown (1) •Satellite Cost Model ( and are both required) – Bus Cost •Cost depends on bus performance level (low, medium, high) – Payload Cost •Cost depends on mission category and performance •Four categories (you can select from – ).

  A cost estimate may also be used to prepare a project cost baseline, which is the milestone-based point of comparison for assessing a project’s actual cost performance. Key Components of a Cost Estimate. A cost estimate is a summation of all the costs involved in successfully finishing a project, from inception to completion (project duration). Launch Systems. Space Manufacturing and Reliability. Cost Modeling. Limits on Mission Design. Design of Low-Cost Spacecraft. Applying the Space Mission Analysis and Design. Estimation Model of Spacecraft Parameters and Cost Based on a Statistical Analysis of COMPASS Designs A model-based approach to the. Cost estimating and cost management tools continue to be developed and will be added to the department’s estimating tool box as they become available. Please note that while cost estimating in support of design-bid-build projects is covered in depth in this manual, there are certain other conditions, such as design-build project delivery. COST AND MASS ESTIMATION MODEL OF SMALL SATELLITES AT SYSTEM DESIGN LEVEL M. Mirshams1), M. Samani2), A. Darabi3) [email protected] samani @ 1) Mechanical and Aerospace Engineering of KNTU 2) 3) Aerospace Research Institute, Ministry of Sciences, Research and Technology ABSTRACT At the end of s, new generation of small satellites were built.

  The aim of this work is to discuss an analytical model capable of estimating, with the accuracy required by a preliminary mission analysis, the performance of a spacecraft equipped with a plasma brake in a (near-circular) low Earth orbit. (and E-sail) system was tried in by the Estonian satellite ESTCube-1 [18,19], but a failure. sionals, and supporting documentation; or deliver preliminary findings. All RAND Small Satellite Cost Model Cost Estimating Relationships for Space-Based Systems: IDA Paper P Spacecraft Functional Cost Estimating Relationships Passive Sensor Cost Model (PSCM). satellite mission costs are primarily driven by technology. For exa m ple, 20Mbit/s X-band transmitters by Axelspace in Japan at 1 kg mass cost $ , because the cost is. RemoveDebris Mission. Platform Launch Mission Status DebrisSats Payload Ground Segment References. RemoveDebris is an EU (European Union) Framework 7 (FP7) research project to develop and fly a low cost in-orbit demonstrator mission that aims to de-risk and verify technologies needed for future ADR (Active Debris Removal) missions. It is not an end-to-end demonstration of a full ADR mission.