The Effects of the Accuracy of Atmospheric Data on the Structural Design Loads of a Typical Launch Vehicle
Abstract
The effects of simulated inaccuracies of meteorological data were investigated with respect to the structural loads of two types of launch vehicles. The effects of inaccuracies ranging from + 10% to - 10% of atmospheric density, atmospheric temperature, windspeed, wind shear and wind shear length were studied. The two launch vehicles used were a liquid propellant boosted vehicle and a relatively small solid propellant boosted vehicle.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 20, 1964
- Accession Number
- AD0437972
Entities
People
- D. E. Hargis
- J. S. Field
Organizations
- The Aerospace Corporation