Calculation Method for Flight Limit Load of V-band Clamp Separation Shock

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概要

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• A simplified calculation method for estimating a flight limit load of the V-band clamp separation shock was established. With this method, the flight limit load is estimated through addition of an appropriate envelope margin to the results acquired with the simplified analysis method proposed in our previous paper. The envelope margin used in the method was calculated based on the reviews on the differences observed between the results of a pyroshock test and the analysis. Using the derived envelope margin, a calculating formula of the flight limit load, which envelopes the actual pyroshock responses with a certain probability, was developed. Based on the formula, flight limit loads for several actual satellites were estimated and compared to the test results. The comparative results showed that the estimated flight limit loads appropriately envelope the test results, which confirmed the effectiveness of the proposed method.

• 一般社団法人 日本機械学会の論文

著者

• Shi Qinzhong

  Japan Aerospace Exploration Agency

• IWASA Takashi

  Tottori University

関連論文

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• Simplified Analysis Model for Predicting Pyroshock Responses on Composite Panel
• Prediction of Acoustically Induced Random Vibration Response of Satellite Equipments with Proposed Asymptotic Apparent Mass
• Calculation Method for Flight Limit Load of V-band Clamp Separation Shock

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