1997
DOI: 10.1117/12.274215
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<title>Payload isolation system for launch vehicles</title>

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Cited by 9 publications
(4 citation statements)
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“…For spacecraft vibration isolation, several developed vibration protection systems (for example, [6,37,43,47,48]) are currently designed and offered in the space services market. They use various workflow management systems in vibration protection systems.…”
Section: The State Of Development Of Vibration Protection Systems For...mentioning
confidence: 99%
See 1 more Smart Citation
“…For spacecraft vibration isolation, several developed vibration protection systems (for example, [6,37,43,47,48]) are currently designed and offered in the space services market. They use various workflow management systems in vibration protection systems.…”
Section: The State Of Development Of Vibration Protection Systems For...mentioning
confidence: 99%
“…Maintaining the operability and operational characteristics of various spacecraft systems [15,20,30,39,48] during their launch into a working orbit and during their operation in orbit is no less difficult design task in comparison with the task of ensuring the integrity and strength of the spacecraft.…”
Section: Introductionmentioning
confidence: 99%
“…Therefore, the multi-leg platform was proposed and studied. Under the auspices of the Phillips Air Force Laboratory in the United States, Wilke et al [15] developed the lateral passive payload adapter IPAF. The experimental results show that the vibration isolation system has a good suppression effect on the lateral vibration load in the range of 25-40 Hz.…”
Section: Introductionmentioning
confidence: 99%
“…Reduction of launch-induced dynamic loads of the spacecraft would greatly reduce the risk that the spacecraft and its components will be damaged during their ascent into orbit, and would also allow more sensitive equipment to be included in missions. As the severe launch environment also accounts for much of the expense of designing, qualifying, and testing spacecraft components, significant cost can also be saved if dynamic responses transmitted to the spacecraft are reduced [1,2].…”
Section: Introductionmentioning
confidence: 99%