Abstract
In order to meet the space transportation needs for a new century, America’s National Aeronautics and Space Administration (NASA) has implemented an Integrated Space Transportation Plan to produce safe, economical, and reliable access to space. One near term objective of this initiative is the design and development of a next-generation vehicle and launch system that will transport crew and cargo to and from the International Space Station (ISS), the Orbital Space Plane (OSP). The OSP system is composed of a manned launch vehicle by an existing Evolved Expendable Launch Vehicle (EELV). The OSP will provide emergency crew rescue from the ISS by 2008, and provide crew and limited cargo transfer to and from the ISS by 2012. A key requirement is for the OSP to be safer and more reliable than the Soyuz and Space Shuttle, which currently provide these capabilities.
NASA has taken an integrated systems approach in designing the OSP launch system and related ground operations and launch support services. This “System-Centric” approach, as opposed to a “Vehicle-Centric” approach, presents unique challenges in terms of meeting the desired safety and reliability requirements As a result, NASA is utilizing PRA, a methodology for quantitative risk assessment, on the entire system during the design process and throughout the life of the system. When PRA is performed early in the design and development cycle with full engineering design and operations involvement, the PRA based integrated system model will provide a means for methodical and objective optimisation of the conceptual design.
This paper discusses the development and implementation of PRA in the OSP Program. The OSP Program is the first major NASA program to perform and use PRA during the concept formulation phase of the program and is expected to produce the paradigm by which future space launch systems can be designed to meet successively higher safety and reliability demands [1].
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
Similar content being viewed by others
References
NASA. Orbital Space Plane Fact Sheet: Beginning a New Era of Space Flight: The Orbital Space Plane. FS-2003-05-64-MSFC, May 2003
NASA. Orbital Space Plane Level II System Requirements Document. MSFC-RQMT-3360, Nov 2003
NASA. Orbital Space Plane Level I Requirements Program Interpretation Document. OSP-DOC-001, Nov 2003
NASA. Probabilistic Risk Assessment Procedures Guide for NASA Mangers and Practitioners. Pending Approval, Aug 2002
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2004 Springer-Verlag London
About this paper
Cite this paper
Rogers, J.H., Safie, F.M., Stott, J.E., Lo, Y. (2004). Application of Probabilistic Risk Assessment (PRA) During Conceptual Design for the NASA Orbital Space Plane (OSP). In: Spitzer, C., Schmocker, U., Dang, V.N. (eds) Probabilistic Safety Assessment and Management. Springer, London. https://doi.org/10.1007/978-0-85729-410-4_313
Download citation
DOI: https://doi.org/10.1007/978-0-85729-410-4_313
Publisher Name: Springer, London
Print ISBN: 978-1-4471-1057-6
Online ISBN: 978-0-85729-410-4
eBook Packages: Springer Book Archive