Loading...
Please wait, while we are loading the content...
Similar Documents
Launch vehicle effluent measurements during the august 20, 1977, titan 3 launch at air force eastern test range
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Woods, D. C. Bendura, R. J. Wornom, D. E. |
| Copyright Year | 1979 |
| Description | Airborne effluent measurements within the launch cloud and visible and infrared measurements of cloud physical behavior are discussed. Airborne effluent measurements include concentrations of HCl, Cl2, NO, NOX, and particulates as a function of time during each sampling pass through the exhaust cloud. The particle size distribution was measured for each pass through the cloud. Mass concentration as a function of particle diameter was measured over the size range of 0.05- to 25 micron diameter, and particle number density was measured as a function of diameter over a size range of 0.5 to 7.5 micron. Effluent concentrations in the cloud ranged from about 30 ppm several minutes after launch to about 1 to 2 ppm at 100 minutes. Maximum Cl2 concentrations were about 40 to 55 ppb and by 20 minutes were less than 1.0 ppb. A tabulated listing of the airborne data is given in the appendix. Usable cloud imaging data were limited to the first 16 minutes after launch. |
| File Size | 1788718 |
| Page Count | 100 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19790007278 |
| Archival Resource Key | ark:/13960/t2h757190 |
| Language | English |
| Publisher Date | 1979-01-01 |
| Access Restriction | Open |
| Subject Keyword | Environment Pollution Test Ranges Chlorine Troposphere Particulates Infrared Spectra Gas Composition Tables Data Concentration Composition Titan 3 Launch Vehicle Hydrogen Chlorides Air Sampling Rocket Exhaust Nitrogen Oxides Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |