Deployment of dishes with surface discontinuities
- 1 July 1996
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 33 (4) , 569-574
- https://doi.org/10.2514/3.26801
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Dynamic deployment of the CRTS reflectorPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1994
- Design and development of a deployable mesh antenna for MUSES-B spacecraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- CONSTRUCTION CONCEPTS FOR PRECISION SEGMENTED REFLECTORSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Technology Assessment and Development of Large Deployable AntennasJournal of Aerospace Engineering, 1993
- Preliminary design considerations for 10-40 meter-diameter precisiontruss reflectorsJournal of Spacecraft and Rockets, 1991
- New deployable truss concepts for large antenna structures or solar concentratorsJournal of Spacecraft and Rockets, 1991
- Concept of the tension truss antennaAIAA Journal, 1990
- Segmented Mirror, Manufacturing And Alignment Tolerances (SMMAT)Published by SPIE-Intl Soc Optical Eng ,1989
- Inflatable space rigidized reflector development for land mobile missionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- The MBB unfurlable mesh antenna (UMA) design and developmentPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986