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  • ...elled reaction mass come in direct contact with the asteroid. The tractor spacecraft could either hover near the object being deflected, or orbit it, directing ...elerating the object as a whole over an extended period of time, using the spacecraft's own mass and associated gravitational field to effect the necessary defle ...
    10 KB (1,518 words) - 06:34, 22 November 2023
  • ...ac.il/~bgusat/CDR.PDF |url-status=dead }}</ref> The students worked on the design of the altitude and control system, the power system and ground station ope ...ith the donation of Rachel and Max Javit from Connecticut, the satellite's design evolved to a 3U CubeSat (30x10x10 cm) with a small Earth observation camer ...
    7 KB (968 words) - 07:52, 12 December 2024
  • == Relevance to spacecraft propulsion == ...MF system as run operated at 350&nbsp;kHz, at 2 MW of power, far below its design rating. ...
    8 KB (1,159 words) - 11:33, 12 December 2023
  • {{Infobox spacecraft class ...器}}) or simply as the '''lunar surface lander''' ({{Lang|zh|月面着陆器}}), is a spacecraft under development by the [[China Academy of Space Technology]]. The purpose ...
    23 KB (3,034 words) - 23:32, 2 March 2025
  • {{Short description|Hypothetical spacecraft propulsion concept using external force fields momentum for transportation} ...ead [[momentum]] of the [[spacecraft]] is changed by an interaction of the spacecraft with external [[Field (physics)|force fields]], such as [[Gravitational fie ...
    14 KB (2,090 words) - 05:13, 15 September 2024
  • ...b|right|Helium vector magnetometer of [[Pioneer 10]] and [[Pioneer 11|11]] spacecraft]] ...lows the magnetometer to make observations with less interference from the spacecraft itself]] ...
    25 KB (3,701 words) - 01:55, 17 October 2024
  • ...e critical need for accurate predictions of aerodynamic heating to protect spacecraft during [[Atmospheric entry|re-entry]], and is considered to be a pioneering ...Heat Flux |url=https://arc.aiaa.org/doi/10.2514/2.3342 |journal=Journal of Spacecraft and Rockets |language=en |volume=35 |issue=3 |pages=403–405 |doi=10.2514/2. ...
    6 KB (845 words) - 05:30, 14 January 2025
  • ...space|power plants]], [[Spacecraft propulsion|propulsion]] or [[Spacecraft|spacecraft systems]] in space. Such space systems require advanced high-temperature [[Spacecraft thermal control|thermal control systems]]. ...
    25 KB (3,571 words) - 13:44, 28 December 2024
  • ...name=Geary>{{cite book|last=Geary|first=Joseph|title=Introduction to Lens Design with Practical ZEMAX Examples|year=2002|publisher=Willmann-Bell|isbn=094339 In the 21st century, the [[New Horizons]] spacecraft, which was an unmanned space probe sent past Pluto and the Kuiper belt, had ...
    3 KB (427 words) - 02:20, 1 August 2023
  • ...t attitude control''' is the process of controlling the orientation of a [[spacecraft]] (vehicle or satellite) with respect to an [[inertial frame of reference]] Before and during attitude control can be performed, '''spacecraft attitude determination''' must be performed, which requires [[sensor]]s for ...
    31 KB (4,599 words) - 03:48, 21 December 2024
  • ==Advantages of the design== ...down in Nuclear Thermal Rockets and Advanced Concepts |journal= Journal of Spacecraft and Rockets|volume=54 |issue=4 |pages=967–972 | date=2017|doi=10.2514/1.A33 ...
    15 KB (2,400 words) - 10:15, 7 January 2024
  • [[File:Helios Dust1.jpg|thumb|Schematic view of the Helios spacecraft with the three photometers (P15, P30, and P90) of the Zodiacal light instru ...characterize the [[Zodiacal dust cloud]] inside the Earth’s orbit down to spacecraft positions 0.3 [[Astronomical unit|AU]] from the sun. The '''''Zodiacal ligh ...
    24 KB (3,566 words) - 23:22, 17 August 2024
  • * [[Collision avoidance (spacecraft)]] ...1">{{Cite book |last1=Hu |first1=Xinyuan |last2=Ye |first2=Naijia |chapter=Design of Active Collision Avoidance Algorithm for Driverless Cars Based on Machin ...
    15 KB (2,075 words) - 08:48, 17 October 2024
  • ...ref name=cdeagle>{{cite web|last=Eagle |first=C. David |title=Frozen Orbit Design |url=http://www.cdeagle.com/omnum/pdf/frozen1.pdf |work=Orbital Mechanics w ...spacecraft in the desired orbit. For a [[Geostationary orbit|geostationary spacecraft]], correction maneuvers on the order of {{cvt|40–50|m/s|mph}} per year are ...
    33 KB (5,290 words) - 08:21, 31 January 2025
  • ...es in and out the atmosphere. '''Glide''' is a flight trajectory where the spacecraft stays in the atmosphere for a sustained flight period of time.<ref name="Sä In June 1939, Kurt Patt of [[Klaus Riedel]]'s design office at Peenemünde proposed wings for converting rocket speed and altitud ...
    22 KB (3,194 words) - 18:20, 23 February 2025
  • {{Infobox spacecraft instrument | Spacecraft = [[Perseverance (rover)|''Perseverance'']] <!--spacecraft it is hosted aboard--> ...
    24 KB (3,321 words) - 13:49, 13 February 2025
  • ...ons.<ref>{{cite book|last=Brown|first=Charles|title=Elements of spacecraft design|year=2002|pages=106|isbn=9781600860515|url=https://books.google.com/books?i ...
    6 KB (889 words) - 05:52, 26 July 2024
  • ...rimary field of engineering concerned with the development of Aircraft and Spacecraft. In the Indian Context previously only the Aeronautical Engineering discipl ...
    8 KB (965 words) - 08:55, 26 January 2025
  • }}</ref> and [[spacecraft]]<ref>{{cite journal |journal= Journal of Spacecraft and Rockets ...
    19 KB (2,648 words) - 01:19, 19 January 2025
  • ...ts can theoretically give high performance, depending on the fuel used and design specifications, and a great deal of research has gone into a variety of typ ...Engine. Advanced launch vehicles |publisher=KBKhA - [[Chemical Automatics Design Bureau]] |url=http://www.kbkha.ru/?p=8&cat=11&prod=66 |accessdate=2009-09-2 ...
    11 KB (1,682 words) - 23:34, 28 November 2024
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