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Design of liquid propellant rocket engines by
Material type: Text Text
Publication details: Washington NASA 1971
Availability: Items available for loan: JRD Tata Memorial Library (1)Call number: 629.475 N71.

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Role of hydrogen injection temperature on the combustion instability of cryogenic rocket engine by K S Biju Kumar by Series: IISc, Dept. of AE, PhD Thesis
Material type: Text Text
Publication details: Bangalore IISc 2012
Availability: Items available for reference: JRD Tata Memorial Library: Not for loan (1)Call number: 621.4361 P12 "THESIS".

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