Khoze Kessaev

Possui graduação em Engineer In Aerospace Engines pela Moscow Aviation Institute(1960), doutorado em Rocket Engines pela Moscow Aviation Institute(1965) e pós-doutorado pela University of Wisconsin-Madison(1973). Atualmente é professor titular da Moscow Aviation Institute. Tem experiência na área de Engenharia Aeroespacial, com ênfase em Propulsão Aeroespacial.

Informações coletadas do Lattes em 28/11/2022

Acadêmico

Formação acadêmica

Doutorado em Rocket Engines

1962 - 1965

Moscow Aviation Institute
Título: Theory of ions generator for ion rocket engine
Orientador: Leonid Latishev
Grande área: Engenharias / Área: Engenharia Aeroespacial / Subárea: Propulsão Aeroespacial / Especialidade: Propulsão de Foguetes. Setores de atividade: Aeronáutica e espaço.

Graduação em Engineer In Aerospace Engines

1954 - 1960

Moscow Aviation Institute

Pós-doutorado

1972 - 1973

Pós-Doutorado. , University of Wisconsin-Madison, UW-Madison, Estados Unidos. , Grande área: Engenharias / Área: Engenharia Aeroespacial / Subárea: Confiabilidade Mecânica de Maquinas / Especialidade: Confiabilidade.

Idiomas

Inglês

Compreende Bem, Fala Bem, Lê Bem, Escreve Bem.

Russo

Compreende Bem, Fala Bem, Lê Bem, Escreve Bem.

Áreas de atuação

Grande área: Engenharias / Área: Engenharia Aeroespacial / Subárea: Propulsão Aeroespacial/Especialidade: Propulsão de Foguetes.

Grande área: Engenharias / Área: Engenharia Aeroespacial / Subárea: Confiabilidade Mecânica de Maquinas/Especialidade: Confiabilidade.

Grande área: Engenharias / Área: Engenharia Aeroespacial / Subárea: Propelentes e Combustão/Especialidade: Propelentes e Combustão.

Grande área: Engenharias / Área: Engenharia Aeroespacial / Subárea: Sistemas Aeroespaciais/Especialidade: Foguetes.

Orientou

Boris Vorobjov

Multiple starting and ignition of liquid rocket engines; 1998; Tese (Doutorado em Rocket Engines) - Moscow Aviation Institute,; Orientador: Khoze Kessaev;

Raif Bakirov

Nonstationary thermal effects in gasdynamical resonator; 1996; Tese (Doutorado em Special Topics Of Liquid Rocket Engines) - Moscow Aviation Institute,; Orientador: Khoze Kessaev;

Nicolay Bactinov

Technology of liquid rocket engines testing; 1992; 0 f; Tese (Doutorado em Rocket Engines) - Moscow Aviation Institute,; Orientador: Khoze Kessaev;

Produções bibliográficas

KESSAEV, K. ; NIWA, M. ; SANTANA JR, A. . Development of a Resonance Igniter for GO2/Kerosene Ignition. AIAA - American Institute of Aeronautics and Astronautics , v. 17, n.4, 2001.
KESSAEV, K. ; NIWA, M. ; SANTANA JR, A. . Modular Ignition System Based on Resonance Igniter. AIAA - American Institute of Aeronautics and Astronautics , 2001.
KESSAEV, K. . Theoretical model of resonance tube. Soviet Aeronautics Alerton Press , Kazan, v. 2, p. 49-52, 1990.
KESSAEV, K. . Thermodynamic of the gas pulsation heating. Moscow Aviation Institute Science Work Collection, Moscow, p. 22-28, 1989.
KESSAEV, K. . Oxigen heating-up inside cavity by entering hydrogen jet. Moscow Aviation Institute Science Work Collection, Moscow, p. 49-52, 1988.
KESSAEV, K. . Chock wave oscillations inside a blinded tube with an underexpanded jet entring. Moscow Aviation Institute Work Collection, Moscow, p. 36-44, 1987.
KESSAEV, K. . The gas heating under cycle compressing inside vessel. Moscow Aviation Institute Science Works Collection, Moscow, p. 15-20, 1986.
KESSAEV, K. . Heating of bottle walls with cyclic compressing of gas inside bottle. Moscow Aviation Institute Science Works Collection, Moscow, p. 13-17, 1985.
KESSAEV, K. ; NOSSATOV, V. . Gaseous screen for a thermal protection. Moscow Aviation Institute Work Collection, Moscow, p. 18-26, 1984.
KESSAEV, K. . Method of development of the propellant mixing and combustion in rocket engine chamber. Moscow Aviation Institute Science Works Collection, Moscow, p. 73-79, 1983.
KESSAEV, K. ; KRICUN, V. . Propellants for rocket engines. Moscow Aviation Institute Science Works Collection, Moscow, p. 11-14, 1982.
KESSAEV, K. . Features of the Ionization in Porous Mediums. Soviet Aeronautics Alerton Press Usa , Kazan, v. 2, p. 45-52, 1965.
KESSAEV, K. ; KURPATENKOV, V. . Liquid Rocket Engine Chamber Calculation. 1. ed. Moscow: MAI Publishing House, 1993. v. 1. 112p .
KESSAEV, K. ; BEREZANSKAIA, E. ; KUDRIAVTSEVA, L. . Thermaldynamical calculation of Burning and Combustion Products Issuing. 1. ed. Moscow: MAI Publishing House, 1993. 75p .
KESSAEV, K. ; KUDRIAVTSEVA, L. . Calculation of Rocket Engines Schemes with Pump Feeding. 1. ed. Moscow: MAI Publishing House, 1990. 96p .
KESSAEV, K. ; KURPATENKOV, V. . Injectors Design for Liquid Rocket Engines. Moscow: MAI Publishing House, 1987. 52p .
KESSAEV, K. ; RIBAKOV, V. . Thermodynamial Properties of Propellants. 1. ed. Moscow: MAI Publishing House, 1987. 50p .
KESSAEV, K. ; KURPATENKOV, V. . Calculation of Combustion Chamber. 1. ed. Moscow: MAI Publishing House, 1985. 96p .
KESSAEV, K. ; KOZLOV, A. . Propellants for Liquid Rocket Engines. 1. ed. Moscow: MAI Publishing House, 1985. 75p .
KESSAEV, K. ; KURPATENKOV, V. ; KUDRIAVTSEVA, L. . The Basic Scheme Parameters of LRE Calculation. Moscow: MAI Publishing House, 1982. 60p .
KESSAEV, K. ; TROFIMOV, R. . Reliability of Rocket Engines. 1. ed. Moscow: Mashinostroeinie, 1982. v. 1. 190p .
KESSAEV, K. ; TROFIMOV, R. . Regression Model of the Turbopump Parameters. 1. ed. Moscow: MAI Publishing House, 1980. 50p .
KESSAEV, K. . The Rocket Thrust as a Function of Nozzle Expansion. 1. ed. Moscow: MAI Publish House, 1977. 54p .
KESSAEV, K. . Reliability of Rocket Engines. 1. ed. Moscow: MAI Publishing House, 1976. 104p .
KESSAEV, K. . Temperature of burning as a function of propellant mixture ratio. 1. ed. Moscow: MAI Publishing House, 1975. 48p .
KESSAEV, K. . Measurement of a heat release with the solid propellant burning. 1. ed. Moscow: MAI Publishing House, 1972. 52p .
KESSAEV, K. ; KOZLOV, A. . Lectures about Rocket Propellants. 1. ed. Moscow: MAI Publishing House, 1971. 58p .
KESSAEV, K. ; NIWA, M. ; SANTANA JR, A. . Torch with oxidizer augmentation for LOX/LH2 engine ignition. In: 36-th AIAA Joint Propulsion Conference and Exhibit, 2000, Huntsville, AL.. AIAA - 2000-3169, 2000.
KESSAEV, K. ; NIWA, M. ; SANTANA JR, A. ; VALLE, M. B. . Development of Resonance Ignitor for GO2/Kerosene Ignition. In: 36-th AIAA Joint Propulsion Conference and Exhibit, 2000, Huntsville, AL.. AIAA-2000-3302, 2000.
KESSAEV, K. ; NIWA, M. ; SANTANA JR, A. ; VIDAL, R. P. . Ignition System for future brazilian thruster. In: 51- st International Astronautical Congress, 2000, Rio de Janeiro. IAF - 00 -S.3.03, 2000.
KESSAEV, K. ; NIWA, M. ; BARBOSA, F. ; LOUZADA JR, M. ; SIKHARULIDZE, Y. ; TAMASHIRO, R. ; PEREIRA, F. . Brazilian Rocket Launcher: a Conception for Performance Improvement. In: 51-st International Astronautical Congress, 2000, Rio de Janeiro. IAF-00-S.2.04, 2000.
KESSAEV, K. ; NIWA, M. ; VILLAS BOAS, Danton. I. F. . Some peculiarities of resonance tube gasdynamical heating. In: 8th Brazilian Congress of thermal engineering and Sciences (ENCIT-2000), 2000, Porto Alegre - RS. S01P41(ENCIT-2000), 2000.
KESSAEV, K. . Ignition of non-hypergolic propellants. In: Third International Symposium on Space Propulsion, 1997, Beijing. Proceeding of the Third International Symposium on Space Propulsion, 1997. v. I. p. 241-249.
KESSAEV, K. ; NIWA, M. ; SHIMOTE, W. K. . VLS1-V02: discussion on failure reason and recomendations on trouble solution 2000 (Technical Report).
KESSAEV, K. . Theory and Calculation of Liquid Rocket Engines 1997 (Manual).
KESSAEV, K. . Gasdynamical igniter Gidder-2M for HM-7 engine (France). Moscow: MAI Administration, 1995 (Technical Report).
KESSAEV, K. . Kerosene gasgenerator ignition by gasdynamical igniter. Moscow: Russia Space Agency Research Center, 1995 (Technical Report).
KESSAEV, K. . Drawing and design justifications of gasdynamical igniter. Moscow: MAI Administration, 1992 (Technical Report).
KESSAEV, K. . The logic and criteria used in the design of gasdynamic igniter. Moscow: MAI Administration, 1991 (Technical Report).

Outras produções

KESSAEV, K. ; ALMEIDA, D. S. . Cutting torch, based on a jet issued from rocket nozzle. 2001.

KESSAEV, K. . GO2/liquid fuel resonance ignition. 2000.

KESSAEV, K. . Modular ignition system for rocket engine. 2000.

KESSAEV, K. . Gasdynamical igniter for Soyuz Rocket. 1998.

KESSAEV, K. . Gasdynamical igniter for Launcher Ricksha. 1997.

KESSAEV, K. . The turn valve. 1996.

KESSAEV, K. . Gasdynamical igniter Gidder-2M for HM-7 engine. 1995.

KESSAEV, K. . Gasdynamical igniter Gidder-1A. 1995.

KESSAEV, K. . Gasdynamical igniter Gidder-2 for HM-7 engine. 1993.

KESSAEV, K. . Gasdynamical igniter Gidder-1. 1992.

KESSAEV, K. . Method of the two-phase propellant ignition. 1990.

KESSAEV, K. . Method of a liquid propellant ignition. 1990.

KESSAEV, K. . Method of the two-component propellant ignition. 1990.

KESSAEV, K. . The gasdynamical igniter. 1990.

KESSAEV, K. ; DEMCHENKO, V. . Method of the two-component ignition. 1989.

KESSAEV, K. . Method of propellant combustion. 1989.

KESSAEV, K. ; NESHIN, A. ; VOLOKOVA, N. . The gasdynamical igniter. 1989.

KESSAEV, K. ; DEMCHENKO, V. . The gasdynamical igniter. 1988.

KESSAEV, K. ; SEMEONOV, V. . The Gasdynamical Igniter. 1986.

KESSAEV, K. ; NESHIN, A. . The gasdynamical igniter. 1986.

KESSAEV, K. . Design and development of the ignition system for european Vinci engine. 1999.

Prêmios

1984

MAI Prize for the book: Reliability of Rocket Engines, MAI administration.

1977

Honorable University Professor, Ministry of Russian State Education.

1960

Graduated with honours as Engineer, Moscow Aviation Institute.

Histórico profissional

Endereço profissional

Centro Técnico Aeroespacial, Instituto de Aeronáutica e Espaço, Asa P. , Praça Mal. Eduardo Gomes, 50, Vila das Acácias, 12228-904 - Sao Jose dos Campos, SP - Brasil, Telefone: (12) 3474768, URL da Homepage:

Experiência profissional

1999 - 2000

Centro Técnico Aeroespacial

Vínculo: Colaborador, Enquadramento Funcional: Pesquisador visitante estrangeiro, Carga horária: 40

Atividades

07/1999
Pesquisa e desenvolvimento , Instituto de Aeronáutica e Espaço, Asa P.,Linhas de pesquisa
07/1999
Serviços técnicos especializados , Instituto de Aeronáutica e Espaço, Asa P.,Serviço realizado, Projeto, construção e teste do ignitor gasdinâmico.
07/1999
Serviços técnicos especializados , Instituto de Aeronáutica e Espaço, Asa P.,Serviço realizado, Projeto, construção e teste do modular ignition system.
07/1999
Serviços técnicos especializados , Instituto de Aeronáutica e Espaço, Asa P.,Serviço realizado, Projeto, construção e teste do cutting torch.
07/1999
Treinamentos ministrados , Instituto de Aeronáutica e Espaço, Asa P.,Treinamentos ministrados, Treinamento do pessoal envolvido no banco de ensios
08/1999 - 09/1999
Outras atividades técnico-científicas , Centre National D'etudes Spatiales Paris France, .,Atividade realizada, Qualified expert for development of the European Engine "VINCI".

1960 - 1966

Moscow Aviation Institute

Vínculo: Outro, Enquadramento Funcional: Scientific researcher, Carga horária: 40

Atividades

11/1991
Serviços técnicos especializados , Engine Department, Theory And Design Of Rocket Engines.,Serviço realizado, Design, development and manufacturing of gasdynamical igniter divices for Société Européenne de Propulsion (France), NPO Energomash (Moscow), Chemiautomatic Design Bureau (Voronez), Russian Space Agency Research Center (Moscow),NPO Energia (Korolev). Cent.
11/1991
Serviços técnicos especializados , Engine Department, Theory And Design Of Rocket Engines.,Serviço realizado, Ignition System expertize for future European Engine "Vinchi" (CNES, France).
11/1991
Outras atividades técnico-científicas , Engine Department, Theory And Design Of Rocket Engines.,Atividade realizada, Joint work and science assistance for Russian and European organizations in the multiple ignition area.
09/1977
Ensino,,Disciplinas ministradas, Theory and calculations of liquid rocket engines, Reliability of liquid rocket engines, Propellants of rocket engines, Introdution in engines speciality, Turbopumps calculations, Solid rocket engines design
09/1977
Ensino, Special Topics Of Liquid Rocket Engines, Nível: Pós-Graduação,Disciplinas ministradas, Ignition and combustion of propellants, Configuration design of liquid rocket engines, Relliability of liquid rocket engines
02/1960
Pesquisa e desenvolvimento , Engine Department, Theory And Design Of Rocket Engines.,Linhas de pesquisa
09/1977 - 09/1998
Extensão universitária , Engine Department, Theory And Design Of Rocket Engines.,Atividade de extensão realizada, Theory and calculation of liquid rocket engines for russian, european and brazilian specialists.
05/1998 - 06/1998
Extensão universitária , Engine Department, Theory And Design Of Rocket Engines.,Atividade de extensão realizada, Practical work with rocket engine for brazilian specialists.
02/1998 - 04/1998
Extensão universitária , Engine Department, Theory And Design Of Rocket Engines.,Atividade de extensão realizada, Calculation of Liquid Rocket Engine for brazilian specialists.
02/1997 - 04/1997
Extensão universitária , Engine Department, Theory And Design Of Rocket Engines.,Atividade de extensão realizada, Theory and calculation of liquid rocket engines for brazilian specialists.
03/1994 - 04/1994
Extensão universitária , Engine Department, Theory And Design Of Rocket Engines.,Atividade de extensão realizada, Ignition of Liquid Propulsion engines for european specialists group.
02/1960 - 09/1966
Pesquisa e desenvolvimento , Engine Department, Theory And Design Of Rocket Engines.,Linhas de pesquisa