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Quality control algorithms and proposed integration process for wind profilers used by launch vehicle systems
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Barbre Jr., Robert E. Decker, Ryan |
| Copyright Year | 2011 |
| Description | Impact of winds to space launch vehicle include Design, Certification Day-of-launch (DOL) steering commands (1)Develop "knockdowns" of load indicators (2) Temporal uncertainty of flight winds. Currently use databases from weather balloons. Includes discrete profiles and profile pair datasets. Issues are : (1)Larger vehicles operate near design limits during ascent 150 discrete profiles per month 110-217 seasonal 2.0 and 3.5-hour pairs Balloon rise time (one hour) and drift (up to 100 n mi) Advantages of the Alternative approach using Doppler Radar Wind Profiler (DRWP) are: (1) Obtain larger sample size (2) Provide flexibility for assessing trajectory changes due to winds (3) Better representation of flight winds. |
| File Size | 200622 |
| Page Count | 10 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20110015754 |
| Archival Resource Key | ark:/13960/t2g78ch1w |
| Language | English |
| Publisher Date | 2011-08-01 |
| Access Restriction | Open |
| Subject Keyword | Space Transportation And Safety Meteorological Radar Algorithms Launch Vehicles Quality Control Wind Profiles Aerospace Safety Doppler Radar Spacecraft Launching Wind Meteorology Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Presentation |
