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Study of solid rocket motors for a space shuttle booster. appendix e: environmental impact statement, solid rocket motor, space shuttle booster
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1972 |
| Description | An analysis of the combustion products resulting from the solid propellant rocket engines of the space shuttle booster is presented. Calculation of the degree of pollution indicates that the only potentially harmful pollutants, carbon monoxide and hydrochloric acid, will be too diluted to constitute a hazard. The mass of products ejected during a launch within the troposphere is insignificant in terms of similar materials that enter the atmosphere from other sources. Noise pollution will not exceed that obtained from the Saturn 5 launch vehicle. |
| File Size | 437384 |
| Page Count | 13 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720015140 |
| Archival Resource Key | ark:/13960/t1pg6ff8f |
| Language | English |
| Publisher Date | 1972-03-15 |
| Access Restriction | Open |
| Subject Keyword | Propulsion Systems Exhaust Gases Air Sampling Solid Propellant Rocket Engines Combustion Products Rocket Exhaust Air Pollution Noise Pollution Space Shuttle Boosters Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
