Loading...
Please wait, while we are loading the content...
Similar Documents
Chemistry of the system: al2o3(c)minus hcl aqueous. [chemical reactions resulting from propellant combustion of rocket propellants
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Tyree Jr., S. Y. |
| Copyright Year | 1975 |
| Description | In order to study exhaust gas chemistry for the space shuttle, the vapor pressure of 2 to 1 weight mixtures of 3-M hydrochloric acid and Al2O3 was studied over a l80 minute reaction period at 31 C. The Al2O3 sample was one of high surface area furnished by NASA Langley Research Center. A brief review is given for aqueous aluminum chemistry, and the chemical reactions of combustion products (exhaust gases) of aluminum propellant binders for the space shuttle are listed. |
| File Size | 9493973 |
| Page Count | 20 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760011160 |
| Archival Resource Key | ark:/13960/t07x15d22 |
| Language | English |
| Publisher Date | 1975-12-14 |
| Access Restriction | Open |
| Subject Keyword | Inorganic And Physical Chemistry Hydrochloric Acid Propellant Binders Rocket Propellants Aqueous Solutions Inorganic Chemistry Exhaust Gases Space Shuttles Aluminum Compounds Chemical Reactions Solid Propellants Propellant Combustion 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 |
