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  • ...n the Apollo 16 and 17 samples and the Lunar-20 sample [1 pg123]. Any ISRU design will have to be able to deal with pyroxene. If we're smart, we'll figure ou
    10 KB (1,417 words) - 07:27, 10 August 2020
  • ...f aluminum oxide would form, which could be an issue for heavy use. Proper design of the engine could mitigate this however. If the combustion was complete a
    12 KB (1,928 words) - 07:04, 18 October 2022
  • ...ate in the ambient vacuum of the moon making various bearings difficult to design.
    12 KB (2,073 words) - 19:58, 6 March 2024
  • ...rted for docks with electrical winches for roll-on/roll-off operations and design for a barge to carry the oversize boosters to Cape Canaveral. We were org
    10 KB (1,664 words) - 08:05, 17 July 2014
  • ( ) Vector substitutes for non-background bitmapped design elements?
    13 KB (1,853 words) - 19:08, 22 June 2019
  • ...White’s efforts to escape made NASA redesign the hatch to a quick release design.
    11 KB (1,900 words) - 05:38, 13 July 2019
  • The main point of this whole design is to get a very large number of Earth people from all over the world invol
    12 KB (2,053 words) - 14:40, 10 April 2019
  • ...eosho, Missouri, with aluminum alloy Domes. My new H-1 Engine Transporter design worked very good for this project. The Engines were shipped to the Cape an
    11 KB (1,800 words) - 08:16, 25 July 2014
  • ...that event that [[Alan B. Binder|Dr. Alan Binder]] came aboard to lead the design study. And the rest is History. [[Lunar Prospector]] orbited the Moon in 19
    13 KB (2,158 words) - 10:14, 30 June 2019
  • ...learned we will be able to pick lunar sites that suit our exact needs and design settlements that are safe and permanent. We will become a space fairing c
    18 KB (3,020 words) - 18:54, 1 August 2007
  • ...re of mole hill construction. Calculations of some of the factors in this design are given in the spreadsheet, MalapertCal0n.xls. The three sections are:
    19 KB (3,316 words) - 00:26, 31 March 2016
  • ...achieve. It would be a natural result of releasing a weight constraint in design and using every means possible to increase exhaust velocity.
    32 KB (5,309 words) - 21:40, 6 March 2024
  • .... This development phase ended with the end of Apollo to the Moon and the design of the Space Shuttle. Since then there has been a steady, but not exponent
    58 KB (9,965 words) - 13:51, 19 October 2022

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