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| Applicability Analysis of Basic Shock Test Condition on Aerocraft External Carry |
| Received:November 14, 2011 |
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| DOI： |
| KeyWord:shock landing shock half-sine pulse terminal peak sawtooth pulse SRS |
| Author | Institution |
| SHI Ming-li |
China Airborne Missile Academy of AVIC，Luoyang，China |
| HUANG Guo-qiang |
China Airborne Missile Academy of AVIC，Luoyang，China |
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| Abstract: |
| The equivalent relation between basic design test condition and landing shock test condition of aerocraft external carry stated in GJB 150.18was analyzed using shock response spectrum theory. The applicability of using basic design test condition for aerocraft external carry was studied. The shock test methods for aerocraft external carry in flight and landing process were put forward. |
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