Thermodynamic aspects of solid propellant gas generator for aircraft application

Bhupesh Parate

Makale detayları

Thermodynamic aspects of solid propellant gas generator for aircraft application

Yazarlar:

Bhupesh Parate

Yayıncı:

Yildiz Technical University

Ana Başlıklar:

Thermodynamics and Statistical Physics

Dergi:

Seatific Journal Vol.3 Issue 1, pp.25-32

Belge Tipi:

Makale

Yayın Tarihi:

6/2023

Belge Dili:

İngilizce

Document ID (Org No.):

2001292587

pISSN:

2792-0771

Anahtar kelimeler:

Özet:

 This research work present mainly on various thermodynamic aspects of solid propellant gas generator for aircraft application. A gas generating device is hot gas generator that creates high temperature and pressure combustion gas on burning of the propellant inside the cartridge case. Thermodynamics is the branch of science which deals with energy transformation into work and vice versa. These devices are filled with energetic materials EMs and used to perform a critical operation in an emergency under adverse conditions. It releases the energy very quickly. Gas generator has a large number of applications and its demand is continuously increasing in the areas of aerospace and aeronautical technologies. A data acquisition system is used to record time to maximum pressure TPmax and maximum pressure Pmax generated in closed vessel CV for solid propellant gas generator. A double base DB propellant is used as medium for gas generation. The purpose of this research paper is to establish the various relationships and to determine various thermodynamic properties for solid propellant gas generator used in aircraft application. Specific heat of propellant varies from 0.25 to 0.35 calg0C, calorimetric value 925 calg, force constant 1052 Jg, co-volume 0.989, flame temperature 2944 K and etc. were experimentally determined.

 This research work present mainly on various thermodynamic aspects of solid propellant gas generator for aircraft application. A gas generating device is hot gas generator that creates high temperature and pressure combustion gas on burning of the propellant inside the cartridge case. Thermodynamics is the branch of science which deals with energy transformation into work and vice versa. These devices are filled with energetic materials EMs and used to perform a critical operation in an emergency under adverse conditions. It releases the energy very quickly. Gas generator has a large number of applications and its demand is continuously increasing in the areas of aerospace and aeronautical technologies. A data acquisition system is used to record time to maximum pressure TPmax and maximum pressure Pmax generated in closed vessel CV for solid propellant gas generator. A double base DB propellant is used as medium for gas generation. The purpose of this research paper is to establish the various relationships and to determine various thermodynamic properties for solid propellant gas generator used in aircraft application. Specific heat of propellant varies from 0.25 to 0.35 calg0C, calorimetric value 925 calg, force constant 1052 Jg, co-volume 0.989, flame temperature 2944 K and etc. were experimentally determined.

 This research work present mainly on various thermodynamic aspects of solid propellant gas generator for aircraft application. A gas generating device is hot gas generator that creates high temperature and pressure combustion gas on burning of the propellant inside the cartridge case. Thermodynamics is the branch of science which deals with energy transformation into work and vice versa. These devices are filled with energetic materials EMs and used to perform a critical operation in an emergency under adverse conditions. It releases the energy very quickly. Gas generator has a large number of applications and its demand is continuously increasing in the areas of aerospace and aeronautical technologies. A data acquisition system is used to record time to maximum pressure TPmax and maximum pressure Pmax generated in closed vessel CV for solid propellant gas generator. A double base DB propellant is used as medium for gas generation. The purpose of this research paper is to establish the various relationships and to determine various thermodynamic properties for solid propellant gas generator used in aircraft application. Specific heat of propellant varies from 0.25 to 0.35 calg0C, calorimetric value 925 calg, force constant 1052 Jg, co-volume 0.989, flame temperature 2944 K and etc. were experimentally determined.

 This research work present mainly on various thermodynamic aspects of solid propellant gas generator for aircraft application. A gas generating device is hot gas generator that creates high temperature and pressure combustion gas on burning of the propellant inside the cartridge case. Thermodynamics is the branch of science which deals with energy transformation into work and vice versa. These devices are filled with energetic materials EMs and used to perform a critical operation in an emergency under adverse conditions. It releases the energy very quickly. Gas generator has a large number of applications and its demand is continuously increasing in the areas of aerospace and aeronautical technologies. A data acquisition system is used to record time to maximum pressure TPmax and maximum pressure Pmax generated in closed vessel CV for solid propellant gas generator. A double base DB propellant is used as medium for gas generation. The purpose of this research paper is to establish the various relationships and to determine various thermodynamic properties for solid propellant gas generator used in aircraft application. Specific heat of propellant varies from 0.25 to 0.35 calg0C, calorimetric value 925 calg, force constant 1052 Jg, co-volume 0.989, flame temperature 2944 K and etc. were experimentally determined.

Makale detayları

Thermodynamic aspects of solid propellant gas generator for aircraft application

Yazarlar:

Bhupesh Parate

Yayıncı:

Yildiz Technical University

Ana Başlıklar:

Thermodynamics and Statistical Physics

Dergi:

Seatific Journal Vol.3 Issue 1, pp.25-32

Belge Tipi:

Makale

Yayın Tarihi:

6/2023

Belge Dili:

İngilizce

Document ID (Org No.):

2001292587

pISSN:

2792-0771

booster

gas generator

propellant

thermodynamics

data acquisition

closed vessel

Sayı

Makale detayları

Thermodynamic aspects of solid propellant gas generator for aircraft application

Yazarlar: Bhupesh Parate

Yayıncı: Yildiz Technical University

Ana Başlıklar: Thermodynamics and Statistical Physics

Dergi: Seatific Journal Vol.3 Issue 1, pp.25-32

Belge Tipi: Makale

Yayın Tarihi: 6/2023

Belge Dili: İngilizce

Document ID (Org No.): 2001292587

pISSN: 2792-0771

booster

gas generator

propellant

thermodynamics

data acquisition

closed vessel

Sayı

Yazarlar:

Bhupesh Parate

Yayıncı:

Yildiz Technical University

Ana Başlıklar:

Thermodynamics and Statistical Physics

Dergi:

Seatific Journal Vol.3 Issue 1, pp.25-32

Belge Tipi:

Makale

Yayın Tarihi:

6/2023

Belge Dili:

İngilizce

Document ID (Org No.):

2001292587

pISSN:

2792-0771