Modeling, Design and Testing of Space Thruster Type Hydrazine Monopropellant for the Low Propulsion and the Application of Satellite Status Change

Q: How can I download an article?

To download an article from SID, first log in to the site, search for the article title, and click on the 'Download Article' option.

Q: How can I download an ISI article?

To download an ISI article on SID, enter the keyword or article title in the search bar, view the relevant results, click on the desired article, and select the 'Download Article' option.

Q: How can I access the SID database?

To access the SID database, visit SID.ir, create an account, and log in to access scientific resources.

Q: Is downloading articles from SID free?

Some articles on SID are available for free, while others require payment. Details are specified on the article's page.

Ebrahim h.; GHANBARI PAKDEHI SH.; ALAVI S.A.

مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources

Journal Paper

Paper Information

Journal: Journal of Iranian Chemical Engineering (Farsi Edition) Year:2022 | Volume:21 | Issue:124 Page(s): 84-106

Download Full-Text

Persian Verion

View:

Download:

Cites:

Information Journal Paper

Title

Modeling, Design and Testing of Space Thruster Type Hydrazine Monopropellant for the Low Propulsion and the Application of Satellite Status Change

Author(s)

Ebrahim h. | GHANBARI PAKDEHI SH. | ALAVI S.A. | Issue Writer Certificate

Keywords

Heterogeneous Decomposition

Modeling

Hydrazine

Adiabatic

Thruster

Monopropellant

Abstract

In the present study, a space Thruster system type Monopropellant has been modeled and designed so as to create a Five-Newton thrust force(propulsion) and specific impulse of 220 seconds, with the usage of adjusting motion or changing the position of the satellite. This model consists of two major parts including a catalytic reactor with Hydrazine feed, 15% nickel catalyst based on gamma alumina and a convergent-divergent nozzle. The catalytic reactor model is a fixed bed, one-dimensional, steady state and Adiabatic with Heterogeneous Decomposition reactions. The process functions by performing two Heterogeneous Decomposition reactions of Hydrazine and ammonia and converting to light gases (hydrogen and nitrogen) with high temperatures. Subsequently, the thrust force will be obtained by the evolution of the gas from bed and nozzle. The catalyst is made up of wet impregnation method and the required characteristics are specified by quantitative, qualitative and thermal analysis tests. The outcomes of modelling include mass, energy, kinetic, physical and chemical variables in the space propulsion. It is also considered as one of the important advantages of designing the measurement and predicting the variables. So as to determine the performance and validity of the model, indicators such as the thrust force, specific impulse, bed pressure drop and the minimum of ammonia decomposition has been scrutinized with the same kinetic and operating conditions in the designing and experimental model (in atmospheric conditions and static). The obtained results are consistent and have been verified.

Cites

No record.

References

No record.

Cite

APA: Copy

Ebrahim, h., GHANBARI PAKDEHI, SH., & ALAVI, S.A.. (2022). Modeling, Design and Testing of Space Thruster Type Hydrazine Monopropellant for the Low Propulsion and the Application of Satellite Status Change. IRANIAN CHEMICAL ENGINEERING JOURNAL, 21(124 ), 84-106. SID. https://sid.ir/paper/1020533/en

Vancouver: Copy

Ebrahim h., GHANBARI PAKDEHI SH., ALAVI S.A.. Modeling, Design and Testing of Space Thruster Type Hydrazine Monopropellant for the Low Propulsion and the Application of Satellite Status Change. IRANIAN CHEMICAL ENGINEERING JOURNAL[Internet]. 2022;21(124 ):84-106. Available from: https://sid.ir/paper/1020533/en

IEEE: Copy

h. Ebrahim, SH. GHANBARI PAKDEHI, and S.A. ALAVI, “Modeling, Design and Testing of Space Thruster Type Hydrazine Monopropellant for the Low Propulsion and the Application of Satellite Status Change,” IRANIAN CHEMICAL ENGINEERING JOURNAL, vol. 21, no. 124 , pp. 84–106, 2022, [Online]. Available: https://sid.ir/paper/1020533/en

Related Journal Papers

No record.

Related Seminar Papers

No record.

Related Plans

No record.

Recommended Workshops