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CFD design and analysis of two Stage ejector for high altitude testing of satellite thrusters

Thesis Info

Author

Hamza Rizwan

Program

MS

Institute

National University of Sciences & Technology

Institute Type

Public

City

Islamabad

Province

Islamabad

Country

Pakistan

Thesis Completing Year

2016

Subject

Science & Technology

Language

English

Added

2021-02-17 19:49:13

Modified

2023-01-06 19:20:37

ARI ID

1676729378398

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