Systems Engineering for the Space Elevator - Complexity

Paper number

IAC-05-D4.3.03

Author

Dr. Laura Pullum, Institute for Scientific Research, Inc., United States

Coauthor

Dr. Peter A. Swan, Teaching Science and Technology, Inc., United States

Year

2005

Abstract

The early goals of the systems engineers of a mega-project, such as a space elevator, are to identify the areas of complexity and establish a methodology to lower the risk and address each issue.  

This paper will present an approach for systems engineering risk identification and identify many of the high-level complexity matrices for the space elevator.  This includes the areas of required basic and applied research.  Some of the areas of investigation are:

   Spacecraft size, propulsion, power, launch, assembly, and deployment

   Ribbon material, design, coatings, size and alternatives  

   Climber velocity, drive motors, and power		

   Politics, such as an international project or involvement with the military

   Environmental issues		

   Tracking issues, such as sensors and communications	  

   Anchor items, such as power 				  

   Power issues, such as laser, beamed RF, conducted RF and locations

The emphasis for this paper is on an approach for systems engineers to take within a mega-project to identify the risks and the complexity issues.  

Abstract document

IAC-05-D4.3.03.pdf

Manuscript document

IAC-05-D4.3.03.pdf (🔒 authorized access only).

To get the manuscript, please contact IAF Secretariat.