Full Record Display for the EPA National Library Catalog


OLS Field Name OLS Field Data
Main Title Design criteria for rocket exhaust scrubbers /
Author Barbarika, Harry. ; Barbarika, Harry F. ; Calvert., Seymour
Other Authors
Author Title of a Work
Calvert, Seymour,
Industrial Environmental Research Laboratory, Research Triangle Park, N. C.
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
Description Access URL
Library Call Number Additional Info Location Last
ELBD RPS EPA 600-7-78-057 repository copy AWBERC Library/Cincinnati,OH 07/31/2018
ESAD  EPA 600-7-78-057 Region 10 Library/Seattle,WA 03/23/2010
NTIS  PB-282 255 Most EPA libraries have a fiche copy filed under the call number shown. Check with individual libraries about paper copy. 06/23/1988
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
OCLC Rec Leader 02533cam 2200505Ii 45010