BUFFETING DATA OBTAINED ON MERCURY/ATLAS MA-2 AND MA-3
Abstract
Two Mercury/Atlas vehicles, MA-2 and MA-3, were instrumented in order to evaluate vehicle structural integrity under flight conditions. The instrumentation system was oriented toward obtaining dynamic rather than static type data since no buffeting data have been obtained on the Mercury configuration. Flight data were obtained through the complete sonic region on MA-2; however, data only up to low transonic region were obtained on MA-3. Structural response data on the adapter and upper LOX tank were obtained. Due to the improper choice of the transducers and ranges, no quantitative data were obtained for adapter vibration and pressure. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 21, 1961
- Accession Number
- AD0268020
Entities
People
- G. Young
- T. Shiokari
Organizations
- The Aerospace Corporation