Venera Images, VENERA 13 fully calibrated image |
Venera Images, VENERA 13 fully calibrated image |
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![]() Senior Member ![]() ![]() ![]() ![]() Group: Members Posts: 1089 Joined: 19-February 05 From: Close to Meudon Observatory in France Member No.: 172 ![]() |
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#2
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![]() Merciless Robot ![]() ![]() ![]() ![]() Group: Admin Posts: 8784 Joined: 8-December 05 From: Los Angeles Member No.: 602 ![]() |
Thanks for sharing this with us, Ralph. In your estimation, were the Veneras on the high or low side of optimum landing configuration (if that makes sense) given your analysis?
-------------------- A few will take this knowledge and use this power of a dream realized as a force for change, an impetus for further discovery to make less ancient dreams real.
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#3
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![]() Member ![]() ![]() ![]() Group: Members Posts: 611 Joined: 23-February 07 From: Occasionally in Columbia, MD Member No.: 1764 ![]() |
In your estimation, were the Veneras on the high or low side of optimum landing configuration (if that makes sense) given your analysis? None of them fell over, so the design can be claimed to be robust. But the question of optimality is meaningless without a stated success criterion (i.e. given an [unknown] surface slope distribution and given an [unknown, but kindof handwavy-estimated here] wind distribution, and given a requirement for e.g. 99% success THEN a certain design can be considered optimal) The fundamental point is that any planetary landing entails uncertainty (qv Philae) and thus no finite-cost design can offer 100% reliability. Thus rational design and evaluation entails the statement of an acceptable degree of risk. Where terrain (or meteorological) factors introduce an entirely stochastic element to the landing dynamics, an optimal mission solution may be to build two 90% landers to achieve an overall 99% chance of safe landing. |
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