Shuttle Fleet Operations: A Simulation Analysis

Abstract

This Note documents a two-part analysis of the reliability of the Space Transportation System (STS). The first part is a strictly statistical examination of the inherent bounds on reliability prediction based on accumulated mission experience as the shuttle program evolves. The results of this analysis suggest that it will take a long history of successes to firmly establish a high shuttle reliability, and that therefore, some contingency provisions should be retained during the early part of the program at least. The second phase of the analysis is aimed at gaining some insight into the operational consequences of less than perfect reliability. This analysis suggests that the risks from the uncertainties surrounding loss or retirement of orbiters, stand-down periods, and delays in refurbishment and turnaround can be reduced by supplementing the four-orbiter STS fleet with additional orbiters or an alternative launch system. Additional keywords: Space missions, Launch vehicles, Statistical analysis, Computations, Confidence intervals, Computerized simulation, Statistical bounds.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1984
Accession Number
ADA151383

Entities

People

  • D. Leinweber

Organizations

  • RAND Corporation

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Accidents
  • Air Force
  • Computer Programs
  • Confidence Limits
  • Data Science
  • High Reliability
  • Launch Vehicles
  • Monte Carlo Method
  • Plastic Explosives
  • Probability
  • Random Variables
  • Reliability
  • Simulations
  • Space Shuttles
  • Space Transportation
  • Statistical Analysis
  • Vehicles

Fields of Study

  • Engineering

Readers

  • Aerospace Engineering.
  • Calculus or Mathematical Analysis
  • Software Engineering

Technology Areas

  • Space