| Main Title |
Design criteria for rocket exhaust scrubbers / |
| Author |
Barbarika, Harry. ;
Barbarika, Harry F. ;
Calvert., Seymour
|
| Other Authors |
|
| CORP Author |
Air Pollution Technology, Inc., San Diego, Calif. ;Air Force Rocket Propulsion Lab., Edwards AFB, Calif.;Industrial Environmental Research Lab., Research Triangle Park, N.C. |
| Publisher |
Environmental Protection Agency, Office of Research and Development, Industrial Research Laboratory ; For sale by the National Technical Information Service, |
| Year Published |
1978 |
| Report Number |
EPA-600/7-78-057; EPA-68-02-2145; EPA-ROAP-21ADL-101 |
| Stock Number |
PB-282 255 |
| OCLC Number |
04277756 |
| ISBN |
pbk. |
| Subjects |
Air--Pollution ;
Solid propellants ;
Solid propellant rockets--Combustion ;
Scrubber (Chemical technology)
|
| Additional Subjects |
Air pollution control ;
Exhaust emissions ;
Scrubbers ;
Rocket exhaust ;
Design criteria ;
Solid rocket propellants ;
Liquid rocket propellants ;
Performance evaluation ;
Hydrogen chloride ;
Hydrogen fluoride ;
Sampling ;
Particles ;
Computer programs ;
Fortran ;
Gas atomized spray scrubbers
|
| Internet Access |
|
| Holdings |
| Library |
Call Number |
Additional Info |
Location |
Last
Modified |
Checkout
Status |
| ELBD ARCHIVE |
EPA 600-7-78-057 |
|
AWBERC Library/Cincinnati,OH |
08/17/2022 |
| ESAD |
EPA 600-7-78-057 |
|
Region 10 Library/Seattle,WA |
03/23/2010 |
| NTIS |
PB-282 255 |
Some EPA libraries have a fiche copy filed under the call number shown. |
|
07/26/2022 |
|
| Collation |
xv, 198 pages : illustrations ; 28 cm. |
| Abstract |
The report gives results of an engineering study and design of methods for scrubbing the exhaust of static-tested solid rockets. Pollutants of major concern were hydrogen chloride and hydrogen fluoride gases. The best process for removing these gases was found to be a gas-atomized spray scrubber, using the power supplied by the rocket to atomize the scrubbing liquid. Four tests in the 22 kN pilot-scale rocket scrubber at the U.S. Air Force Propulsion Laboratory were analyzed to aid in the design. Two types of gas-atomized scrubbers were designed: one was a conventional design similar to a venturi; the other was a low-cost unconventional open type, using neither pressure piping nor a ducted spray chamber. Cost analyses were made for both types of rockets with thrusts between 20 kN and 2 MN. |
| Notes |
Prepared for U.S. Environmental Protection Agency, Office of Research and Development and U.S. Air Force Rocket Propulsion Laboratory, under contract no. 68-02-2145 ROAP 21ADL-101, program element no. 1AB012. Issued Mar. 1978. Includes bibliographical references (pages 180-183). |
| Place Published |
Research Triangle Park, N.C. Springfield, Va. |
| Supplementary Notes |
Prepared for Air Force Rocket Propulsion Lab., Edwards AFB, Calif. |
| Corporate Au Added Ent |
United States. Environmental Protection Agency. Office of Research and Development Air Force Propulsion Laboratory. |
| Corp Au Ser Add Ent |
United States. Environmental Protection Agency. EPA-600/7-78-059. |
| NTIS Title Notes |
Final rept. Dec 75-Dec 77. |
| PUB Date Free Form |
1978 |
| Series Title Untraced |
Interagency energy-environment research and development program report ; EPA-600/7-78-057 |
| Category Codes |
13B; 68A |
| NTIS Prices |
PC A10/MF A01 |
| Primary Description |
600/13 |
| BIB Level |
m |
| Medium |
unmediated |
| Content |
text |
| Carrier |
volume |
| Cataloging Source |
OCLC/T |
| Control Number |
323743455 |
| OCLC Time Stamp |
20180726085957 |
| Language |
eng |
| SUDOCS Number |
EP 1.23/8:600/7-78-057 |
| Origin |
OCLC |
| Type |
MERGE |
| OCLC Rec Leader |
02533cam 2200505Ii 45010 |
