analysis and modification of historical united states spaceflight capsule designs for implementation in future commercial launches
- Paper number
IAC-10,B3,1,9,x7967
- Author
Mrs. Ashley Anderson, University of Alabama in Huntsville, United States
- Year
2010
- Abstract
In fulfillment of the requirements of a senior Mechanical and Aerospace Engineering (MAE) capstone design class at the University of Alabama in Huntsville (UAH) a review and analysis of past United States (US) spaceflight capsule designs has been conducted. Additionally, recommendations are made for future capsule designs with a focus upon the structural design, interior space, astronaut safety, and ergonomics of the capsules. Attention is focused upon ocean splash-down recovery after re-entry of the space capsule from Low Earth Orbit (LEO). This type of landing was utilized on all prior United States (US) spaceflight missions and was not perfected to optimal conditions that ensure astronaut safety. Despite the issues, errors, and failures associated with the past capsules there is a movement back to capsule utilization in both the commercial and private sector, such as NASA‟s Orion Program. The present paper describes the past problems, errors, and design flaws pertaining to the Mercury, Apollo and Gemini capsules. Additionally, a review is provided regarding how the Orion capsule has been designed to remedy past problems and why it is the most viable replacement to the space shuttle. Finally, it is proven that the space capsule can be the most efficient spaceflight tool based on cost, design, testing, safety, and ergonomics.
- Abstract document
- Manuscript document
IAC-10.B3.1.9.pdf (🔒 authorized access only).
To get the manuscript, please contact IAF Secretariat.