This paper discusses the System Safety approach used to assess risk for the Space Shuttle Reusable Solid Rocket Motor (RSRM). Previous to the first RSRM flight in the fall of 1988, all systems were analyzed extensively to assure that hazards were identified, assessed and that the baseline risk was understood and appropriately communicated. Since the original RSRM baseline was established, Thiokol and NASA have implemented a number of initiatives that have further improved the RSRM. The robust design, completion of rigorous testing and flight success of the RSRM has resulted in a wise reluctance to make changes. One of the primary assessments required to accompany the documentation of each proposed change and aid in the decision making proce...
Thesis: M.B.A., Massachusetts Institute of Technology, Sloan School of Management, in conjunction wi...
The executive summary offers a concise overview of the thesis research conducted, focusing on enabli...
Safety will be a major consideration in the operation of Reusable Launch Vehicles (RLVs), regardless...
As part of NASA's intensive effort to incorporate quantitative risk assessment (QRA) tools in the Ag...
This paper presents an overview of the application of the quantitative risk assessment (QRA) methods...
A number of inventors and entrepreneurs are currently attempting to develop and commercially operate...
Since the Shuttle Challenger accident in 1986, communities across National Aeronautic and Space Admi...
Present software development accomplishments are indicative of the emerging interest in and increasi...
NASA has come a long way in our journey to reduce the risks of operating the Spse Shuttle system. Th...
Managers seeking to assess risk within complex systems face enormous challenges. They must identify ...
The SSME when developed in the 1970's was a technological leap in space launch propulsion system des...
A rocket engine safety system was designed to initiate control procedures to minimize damage to the ...
In response to a request from the House of Representatives Committee on Science, Space, and Technolo...
Thesis: S.M. in Engineering and Management, Massachusetts Institute of Technology, System Design and...
Purpose - The main objective of this paper is to introduce the development of a decision-support env...
Thesis: M.B.A., Massachusetts Institute of Technology, Sloan School of Management, in conjunction wi...
The executive summary offers a concise overview of the thesis research conducted, focusing on enabli...
Safety will be a major consideration in the operation of Reusable Launch Vehicles (RLVs), regardless...
As part of NASA's intensive effort to incorporate quantitative risk assessment (QRA) tools in the Ag...
This paper presents an overview of the application of the quantitative risk assessment (QRA) methods...
A number of inventors and entrepreneurs are currently attempting to develop and commercially operate...
Since the Shuttle Challenger accident in 1986, communities across National Aeronautic and Space Admi...
Present software development accomplishments are indicative of the emerging interest in and increasi...
NASA has come a long way in our journey to reduce the risks of operating the Spse Shuttle system. Th...
Managers seeking to assess risk within complex systems face enormous challenges. They must identify ...
The SSME when developed in the 1970's was a technological leap in space launch propulsion system des...
A rocket engine safety system was designed to initiate control procedures to minimize damage to the ...
In response to a request from the House of Representatives Committee on Science, Space, and Technolo...
Thesis: S.M. in Engineering and Management, Massachusetts Institute of Technology, System Design and...
Purpose - The main objective of this paper is to introduce the development of a decision-support env...
Thesis: M.B.A., Massachusetts Institute of Technology, Sloan School of Management, in conjunction wi...
The executive summary offers a concise overview of the thesis research conducted, focusing on enabli...
Safety will be a major consideration in the operation of Reusable Launch Vehicles (RLVs), regardless...