Mechanical Properties of Silicone Elastomer Seals for Space Docking Vehicles
- 1. Beijing Institute of Astronautical Systems Engineering, Beijing (China)
Description
Low impact docking mechanisms (LIDM) are developing. The LIDM seal is one of the key components of the LIDM, and play very critical roles during the docking and berthing of space vehicles. Due to the severe functional requirements, it is difficult to develop the LIDM seal that is a silicone elastomer seal. The excellent mechanical property is firstly required for the LIDM seal. Five design schemes of the LIDM seal are proposed by this paper, and their mechanical properties are studied by the proposed finite element method. The mechanical properties of the LIDM seal have important impacts on the required sealing performance, docking feature and separation feature. The findings are beneficial for the development of the LIDM seal for space docking vehicles. (paper)
Availability note (English)
Available from http://dx.doi.org/10.1088/1757-899X/408/1/012010Additional details
Identifiers
Publishing Information
- Journal Title
- IOP Conference Series. Materials Science and Engineering (Online)
- Journal Volume
- 408
- Journal Issue
- 1
- Journal Page Range
- [6 p.]
- ISSN
- 1757-899X
Conference
- Title
- 2. International Conference on Advanced Technologies in Design, Mechanical and Aeronautical Engineering
- Acronym
- ATDMAE 2018
- Dates
- 1-3 Jul 2018
- Place
- Dalian (China)
INIS
- Country of Publication
- United Kingdom
- Country of Input or Organization
- International Atomic Energy Agency (IAEA)
- INIS RN
- 52094551
- Subject category
- S36: MATERIALS SCIENCE; S42: ENGINEERING;
- Resource subtype / Literary indicator
- Conference
- Descriptors DEI
- DESIGN; ELASTOMERS; FINITE ELEMENT METHOD; MECHANICAL PROPERTIES; PERFORMANCE; SEALS; SILICONES; SPACE; SPACE VEHICLES
- Descriptors DEC
- CALCULATION METHODS; MATHEMATICAL SOLUTIONS; NUMERICAL SOLUTION; ORGANIC COMPOUNDS; ORGANIC SILICON COMPOUNDS; POLYMERS; SILOXANES; VEHICLES