...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
