8 research outputs found

    Convolution Integral Methods for the Computation of Linear Burn Rate of Solid Propellant Subjected to Arbitrary Pressure Excitation

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    400N class thruster operations with hydrazine fuel

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    SIGLEAvailable from British Library Document Supply Centre- DSC:3425.9293(ESA-CR-(X)--3350) / BLDSC - British Library Document Supply CentreGBUnited Kingdo

    ATE advanced technology engine Definition study phase 2; executive summary report

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    Report produced under contract to the European Space AgencySIGLEAvailable from British Library Document Supply Centre-DSC:3425.929300(ESA-CR(X)--4013) / BLDSC - British Library Document Supply CentreGBUnited Kingdo

    Solid Propellant Bibliography

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