Accession Number : ADA314354
Title : Modeling Solid Rocket Booster Exhaust Plumes in the Stratosphere with SURFACE CHEMKIN.
Descriptive Note : Technical rept.,
Corporate Author : AEROSPACE CORP EL SEGUNDO CA
Personal Author(s) : Brady, B. B. ; Martin, L. R.
PDF Url : ADA314354
Report Date : 01 SEP 1995
Pagination or Media Count : 36
Abstract : The results of a detailed chemical model of the transient stratospheric chemistry following passage of a large solid rocket booster motor is described. The model is based on SURFACE CHEMKIN, which is a newly developed multiphase chemical kinetic model. The model incorporates 34 chemical species and over 100 gas phase, heterogeneous, and photochemical reactions. The results show that passage of a Titan IV-sized rocket should produce an ozone 'hole' 10 km in diameter at 20 km altitude, and 28 km in diameter at 30 km altitude, lasting from a few hours to a day. The size and persistence of the hole are very sensitive to the rate of dissipation of the rocket plume, which is poorly understood at present.
Descriptors : *EXHAUST PLUMES, *BOOSTER ROCKET ENGINES, *ROCKET EXHAUST, REACTION KINETICS, PHOTOCHEMICAL REACTIONS, PHASE, SURFACES, CHEMICAL REACTIONS, STRATOSPHERE.
Subject Categories : Rocket Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE