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Massachusetts Institute of Technology

Assessing the fractionated spacecraft concept

Abstract

dc:description.abstract

In the traditional approach, spacecraft are tailored to each mission and are associated with high risks and costs and long cycles. Moreover, once launched, their flexibility remains limited. The concept of spacecraft fractionation could enable manufacturers and users to decrease these risks and costs and to increase space systems flexibility. Fractionation transforms the traditional monolithic spacecraft into a network of elements: a free-flying payload module is supported by free-flying modules that provide the payload with power, communications, etc. Thus modules could be maintained, exchanged, and reused once launched. Furthermore one could imagine developing a whole on-orbit infrastructure made of standardized modules that could support different payloads. This thesis investigates under what conditions fractionated spacecraft could be worthwhile alternatives to traditional ones. The first part assesses different fractionated architectures and compares them with traditional ones in terms of utility and cost for a given mission and given level of performance. A framework based on Multi-Attribute Tradespace Exploration was used to analyze the impact of fractionation, first at spacecraft level for a single mission, and second, at infrastructure level, when the spacecraft is part of the infrastructure.

Degree

thesis:*
Department dc:contributor.department
Massachusetts Institute of Technology. Engineering Systems Division
Grantor dc:publisher
Massachusetts Institute of Technology
Year dc:date.issued
2006

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Mathieu, Charlotte
Advisor dc:contributor.advisor
  • Annalisa L. Weigel.

Subjects

dc:subject × 1

Rights

dc:rights
Statement dc:rights
  • M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.
Language dc:language.iso
eng

Identifiers

dc:identifier.*
Handle dc:identifier.uri
http://hdl.handle.net/1721.1/34522
OAI identifier oai:identifier
oai:dspace.mit.edu:1721.1/34522

Chain of custody

source
Harvested from
MIT
Base URL
dspace.mit.edu/oai/request
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
citation

Mathieu, Charlotte. Assessing the fractionated spacecraft concept. Massachusetts Institute of Technology, 2006. http://hdl.handle.net/1721.1/34522