Please use this identifier to cite or link to this item: http://hdl.handle.net/10603/430429
Full metadata record
DC FieldValueLanguage
dc.coverage.spatial
dc.date.accessioned2022-12-23T10:50:46Z-
dc.date.available2022-12-23T10:50:46Z-
dc.identifier.urihttp://hdl.handle.net/10603/430429-
dc.description.abstractMonopropellants are widely used for propulsion and gas generation applications. The current state of art monopropellant systems are based on hydrazine propellants. While hydrazine has a strong heritage as a versatile monopropellant, some of the inherent problems associated with hydrazine like toxicity, high vapor pressure and associated storage and handling cost have been a major concern. These concerns led to the exploration of nontoxic and better performing alternate propellants, among which Hydroxylammonium Nitrate (HAN) is a promising candidate and scores over other monopropellants in terms of insensitivity, toxicity and volatility. Some of the other projected advantages of HAN formulations over hydrazine include its lower crystallization point, higher density and volumetric impulse. The current practice of decomposing HAN is based on available technology used for hydrazine decomposition. However main challenges for HAN thrusters in contrast to hydrazine are material constraints imposed by the higher temperature levels experienced in HAN thrusters and need of high temperature tolerant catalysts. The catalysts under consideration should be both temperature tolerant and resistant to any possible poisoning from the decomposition products of HAN. There have been few reports of late on the development of suitable catalysts for HAN. Besides, unlike hydrazine, HAN propellants are multi-component, undergoes multistage decomposition adding complexity to the decomposition mechanism. Current work pertains to the development of a high temperature tolerant active catalyst for HAN decomposition. The issues related to catalyst design, catalyst characterization, reactivity to HAN based monopropellants, performance estimation and its decomposition kinetics are extensively pursued in this work. Special tests were developed to measure catalyst s capability to sustain extreme chemical and thermal conditions witnessed in HAN thruster. A novel cobalt doped cerium oxide (CeCo) catalyst was prepared via co-precipitation route...
dc.format.extentxvi, 173p.
dc.languageEnglish
dc.relation
dc.rightsuniversity
dc.titleCerium Oxide Based Active Catalyst for Green Hydroxylammonium Nitrate HAN Fueled Monopropellant Thruster
dc.title.alternative
dc.creator.researcherAgnihotri, Ruchika
dc.subject.keywordEngineering
dc.subject.keywordEngineering Aerospace
dc.subject.keywordEngineering and Technology
dc.description.note
dc.contributor.guideOommen, Charlie
dc.publisher.placeBangalore
dc.publisher.universityIndian Institute of Science Bangalore
dc.publisher.institutionAerospace Engineering
dc.date.registered
dc.date.completed2019
dc.date.awarded2019
dc.format.dimensions30 cm.
dc.format.accompanyingmaterialNone
dc.source.universityUniversity
dc.type.degreePh.D.
Appears in Departments:Aerospace Engineering

Files in This Item:
File Description SizeFormat 
01_title.pdfAttached File95.77 kBAdobe PDFView/Open
02_prelim page.pdf256.42 kBAdobe PDFView/Open
03_table of content.pdf124.69 kBAdobe PDFView/Open
04_abstract.pdf117.38 kBAdobe PDFView/Open
05_chapter 1.pdf427.22 kBAdobe PDFView/Open
06_chapter 2.pdf1.81 MBAdobe PDFView/Open
07_chapter 3.pdf18.85 MBAdobe PDFView/Open
08_chapter 4.pdf5.84 MBAdobe PDFView/Open
09_chapter 5.pdf6.14 MBAdobe PDFView/Open
10_chapter 6.pdf28.42 MBAdobe PDFView/Open
11_annexure.pdf266.82 kBAdobe PDFView/Open
80_recommendation.pdf215.56 kBAdobe PDFView/Open


Items in Shodhganga are licensed under Creative Commons Licence Attribution-NonCommercial-ShareAlike 4.0 International (CC BY-NC-SA 4.0).

Altmetric Badge: