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UID:0-453@aerospace.technion.ac.il

DTSTART;TZID=Asia/Jerusalem:20170222T163000

DTEND;TZID=Asia/Jerusalem:20170222T173000

DTSTAMP:20230603T190449Z

URL:https://aerospace.technion.ac.il/events/spalo-solid-propellant-augment
 ed-by-a-liquid-oxidizer-from-vision-to-reality/

SUMMARY:SPALO – Solid Propellant Augmented by a Liquid Oxidizer: from vis
 ion to reality...
DESCRIPTION:Lecturer:Yoash Mor\n Faculty:Department of Aerospace Engineerin
 g\n Institute:Technion – Israel Institute of Technology\n Location:Class
 room 165\, ground floor\, Library\, Aerospace Eng.\n Zoom: \n Abstract: \n
  Details: \n The SPALO is a new class of solid propellants\, augmented by 
 storable liquid oxidizers. Their structure is similar to conventional soli
 d propellants\; however\, instead of solid oxidizer particles they contain
  small liquid oxidizer units. Thus\, the SPALO behaves like a solid propel
 lant\, but its Isp is higher by 10% and more compared to conventional soli
 d propellants\, indicating a potential to be the next “big thing” in t
 he propulsion field.\nThis research aims to promote the SPALO concept towa
 rds a real propellant. Various chemical and mechanical methods to produce 
 these small liquid oxidizer units have been investigated. We have found a 
 number of ways to lock the liquid oxidizer\, as will be presented.\nA majo
 r outcome of this research is a novel powerful theoretical formulation and
  calculation tool – a Modified Thermal Resistance Model (MTRM). The MTRM
  enables solving relatively easily one-dimensional\, quasi-steady heat tra
 nsfer problems involving heat sources from chemical reactions or phase tra
 nsition\, using thermal resistors. Solution of combustion of a liquid drop
 let and a liquid fuel contained within a porous particle will be demonstra
 ted.
CATEGORIES:Seminars
LOCATION:Classroom 165\, ground floor\, Library\, Aerospace Eng.

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DTSTART:20161030T010000

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