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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
  • ...ume; mass production of such water mining craft would amortize the initial design investment and tooling over hundreds of trips.
    7 KB (1,103 words) - 18:10, 25 May 2019
  • *Kroll, Gustav A. - Group(4) MSFC R-P&VE-S Structures Design 4610 *Milde, Hans W. - Group(4) MSFC R-ASTR-GDA Design Section 4487
    13 KB (2,026 words) - 18:01, 23 July 2014
  • ...tenna, but is certainly an issue which needs to be addressed in the system design. The problem of radio interference is solvable. ...istance from GEO to Earth (40,000 km), so it will validate the engineering design well, and prove that useful power can be beamed over that distance.
    16 KB (2,652 words) - 21:00, 17 July 2009
  • ...tion, but the precise thickness would be determined through an engineering design study.
    7 KB (1,216 words) - 18:50, 10 September 2014
  • ...perations, and in particular the "New Vision" for space. Consider the many design changes the [[ISS into the Pacific|ISS]] when through in the 1990’s and p ...of the bellows to hold the bellows in place. It is certainly possible to design such slides so that they will nest together without taking up to much space
    16 KB (2,566 words) - 19:19, 4 June 2013
  • I reported to Mr. Kuers to get his signature for the rocket being built to design drawings. As he was signing, he asked me to take him to the roll out. I loo
    7 KB (1,223 words) - 19:14, 16 July 2014
  • ...nsolata''', which has two FOSS fonts and was used on our 2013-2018 website design (Coriolis).
    10 KB (1,295 words) - 19:22, 24 March 2021
  • ...urrently in service || [http://www.russianspaceweb.com/zenit.html Yuzhnoe Design Bureau] (see also [http://www.sea-launch.com/ Sea Launch] ||
    16 KB (1,962 words) - 15:23, 9 December 2010
  • ...tain was home to one of, if not the leading companies in the world for the design and creation of small satellites.
    8 KB (1,327 words) - 05:40, 13 July 2019
  • ...ed from L1 to GEO to feed a terrestrial ground based rectenna. The antenna design for L-1 to Luna will work equally well from GEO to Earth
    8 KB (1,343 words) - 14:35, 12 June 2013
  • ...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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