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  • ...vements he had made on the rocket vehicle. I used his electrical harness design modifications for electrical connectors on all future engines.
    6 KB (1,154 words) - 20:44, 18 July 2014
  • ...can be improved in efficiency by careful choice of electrode material and design. Also, performing electrolysis on water at very high temperatures results i
    4 KB (604 words) - 14:29, 19 January 2021
  • ...nsolata''', which has two FOSS fonts and was used on our 2013-2018 website design (Coriolis).
    5 KB (733 words) - 05:29, 26 March 2021
  • It is probably too late for design changes in the ISS, but avoiding rotary joints with electrically conducting
    4 KB (620 words) - 21:58, 15 November 2013
  • Strangelv says, "Mike ponders a throwaway rover design as a followup to the microwave project" ...n't think a mere garage would be big enough once it got beyond the initial design stage."
    13 KB (2,153 words) - 11:43, 14 January 2009
  • ...s means that the lunar landers must carry additional fuel. The new lander design has large fuel tanks for this reason. Also there will be fewer and more li
    4 KB (689 words) - 10:11, 24 April 2012
  • ...pment would require expensive launch on rockets to orbit, but the cost of design and fabrication for things launched into orbit is usually a number of times
    5 KB (787 words) - 11:11, 15 November 2010
  • This suggests an X-Prize rover design as a sandworm. The rover would be snake like, at least as big around as yo ...gn will be very challenging work in robotics. The major concerns for this design are managing the Lilly pad tail and digging deep enough as the regolith get
    14 KB (2,278 words) - 05:04, 30 March 2008
  • [[File:externalspacesuit.jpg|right|thumb|NASA's New Moon Rover Design]]
    5 KB (937 words) - 17:30, 23 June 2013
  • ...A completely indoor operation of the aircraft would simplify a number of design considerations for the blimp itself.
    5 KB (818 words) - 12:53, 12 February 2018
  • ...like California. The risk is there and we must take it into account in the design of the settlement, but it is '''not''' one of our [[Show Stoppers]]. In fac ...ent on the moon again is real and must be addressed in both infrastructure design and operational procedures. It is comparable to the risk of storm damage on
    12 KB (2,192 words) - 04:58, 19 May 2007
  • ...sion Designs and Options]] -- not presently existing reference missions to design<BR/>
    8 KB (1,125 words) - 17:28, 20 June 2019
  • The new Lunar Lander design carries much larger fuel tanks than [[Apollo]]. This gives it both the cap
    5 KB (818 words) - 10:37, 25 February 2013
  • ...ommon/Main Materials Used to Handle Fluorine'''<ref>(P. S. Gakle, et al., "Design Handbook for Liquid Fluorine Ground Handling Equipment, Aerojet-General Cor
    5 KB (722 words) - 10:27, 13 May 2023
  • ...Cape. The project was led by Project Engineer, Hugh King, of the PV&E Lab Design Engineering Section.
    5 KB (894 words) - 21:29, 8 August 2014
  • ...These early missions will test the technologies and capabilities needed to design manned landers. "NASA will look at a number of factors including technical
    5 KB (779 words) - 18:38, 23 June 2019
  • ...open to out-of-box thinking. This entry is part of a new lunar settlement design and is a discussion of how the concept of symbiosis applies to our vision o We need to design a new direction for lunar settlement. To do this we must learn to think ou
    33 KB (5,344 words) - 16:51, 20 January 2012
  • ...ers.edu/~benaroya/publications/Ruess%20et%20al%20ASCE%20JAE.pdf Structural Design of a Lunar Habitat - Journal of Aerospace Engineering, July 2006, pg 137] .
    6 KB (947 words) - 15:46, 10 April 2019
  • :*Select design objectives
    5 KB (747 words) - 20:33, 15 August 2012
  • ...provide all our shielding, see [[Architecture List]]. Any lunar settlement design that does not address the radiation problem should simply be rejected as un
    7 KB (1,101 words) - 09:57, 27 April 2013

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