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Titolo:
SOLID ROCKET EXHAUST IN THE STRATOSPHERE - PLUME DIFFUSION AND CHEMICAL-REACTIONS
Autore:
DENISON MR; LAMB JJ; BJORNDAHL WD; WONG EY; LOHN PD;
Indirizzi:
TRW CO INC,DEPT CHEM TECHNOL REDONDO BEACH CA 90278 TRW CO INC,DEPT FLUID & THERMOPHYS REDONDO BEACH CA 90278 TRW CO INC,DEPT MAT & PROC REDONDO BEACH CA 90278
Titolo Testata:
Journal of spacecraft and rockets
fascicolo: 3, volume: 31, anno: 1994,
pagine: 435 - 442
SICI:
0022-4650(1994)31:3<435:SREITS>2.0.ZU;2-O
Fonte:
ISI
Lingua:
ENG
Soggetto:
KINETIC DATA-BASE; COMBUSTION; CHEMISTRY;
Tipo documento:
Article
Natura:
Periodico
Settore Disciplinare:
Science Citation Index Expanded
Citazioni:
30
Recensione:
Indirizzi per estratti:
Citazione:
M.R. Denison et al., "SOLID ROCKET EXHAUST IN THE STRATOSPHERE - PLUME DIFFUSION AND CHEMICAL-REACTIONS", Journal of spacecraft and rockets, 31(3), 1994, pp. 435-442

Abstract

A model has been developed to examine, on a local scale, the reactions of rocket exhaust from solid rocket motors with stratospheric ozone. The effects were examined at two different altitudes. Results of the modeling study indicate that afterburning chemistry of reactive exhaust products can cause local but transient (on the order of several minutes) loss of ozone. The modeling study included potential heterogeneous reactions at aluminum oxide surfaces. Results indicate that these potential heterogeneous reactions do not have a major impact on the local plume chemistry. Homogeneous reactions appear to be of more consequence during the early dispersion of the plume. It has also been found that the rate of plume dispersion has a very significant effect on local ozone loss.

ASDD Area Sistemi Dipartimentali e Documentali, Università di Bologna, Catalogo delle riviste ed altri periodici
Documento generato il 02/06/20 alle ore 02:03:51