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Beginning in June 2012, an MSSL-led team have performed a study of the requirements and design of a Lunar Surface Camera Package for Exploration L- CAM for the ESA Lunar Lander. However, the Lunar Lander program was terminated by the ESA Ministerial Council in November 2012. As a result, with four of the six TNs requested in the SoW completed, ESA instructed MSSL to concentrate work on the L-CAM thermal model. The following final report is therefore composed of TNs 1- 4 and the Thermal Report.
University College London
The main goals of the DPEM project was [RD1] "to set the foundations for the development of a comprehensive suite of near surface dusty plasma environment models applicable in particular (but not only) to airless bodies of interest for future exploration missions such as asteroids, the Moon, Phobos and Deimos, etc … These models shall allow the definition of charged dust environment specifications to assess the effects of dusty plasmas on near surface or surface exploration units (spacecraft, payload, lander, astronaut) in a surface-spacecraft-dust environment system."
Finnish Meteorological...
Space capsule crew injury protection from landing forces originated from research originally conducted into fast jet ejection. There, the primary focus was on the protection of the pilot’s spine from over-compression and led to the one-dimensional Dynamic Response Index (DRI) for assessing the spinal injury potential of measured acceleration pulses.
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