...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
