Development of a Cold Gas Propulsion System for the ... - SSL - MIT

Development of a Cold Gas Propulsion System for the ... - SSL - MIT Development of a Cold Gas Propulsion System for the ... - SSL - MIT

26.12.2012 Views

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1 Introduction The TALARIS (Terrestrial Artificial Lunar And Reduced gravIty Simulator) hopper is a small prototype flying vehicle designed to serve as an Earth-based testbed for guidance, navigation, and control (GNC) algorithms that will be used to explore lunar and other planetary surfaces. To date, nearly all robotic exploration on the surface of the Moon and other planets has been done by stationary landers or wheeled rovers. Hoppers would open up new modes of exploration with their alternate form of mobility. However, because they are a new technology without the long heritage of landers and rovers, there is a greater need for testing to reduce the risk associated with hoppers. The TALARIS testbed provides the opportunity to develop and mature hopper-based GNC algorithms on Earth, which allows for a more controlled environment and easier human access for modifications, upgrades, and repairs if necessary. A hop consists of three main phases: propulsive ascent, traverse flight, and soft landing. A commanded maneuver of this type has been performed off the Earth once, by the Surveyor 6 spacecraft on the Moon. On November 17, 1967, after Surveyor 6 had been sitting on the lunar surface for a week, the spacecraft’s three liquid-fueled vernier rocket engines were reignited and fired for 2.5 s [1]. The control system was set such that the spacecraft would tilt 7° to the west upon liftoff, and the thrust generated was sufficient to cause the spacecraft to rise to an altitude of about 3.5 m and to land 2.4 m away from its starting point. This allowed Surveyor 6 to send back images of the surface disturbances at its initial landing site, providing information on mechanical properties of the lunar surface as well as the effects of firing rocket engines near the surface. Furthermore, the displacement of the spacecraft provided a baseline for stereoscopic viewing and photogrammetric mapping of the surrounding lunar terrain [1]. However, the Surveyor 6 hop is merely the tip of the iceberg in terms of the potential value that could be gained from exploring with hoppers. Hoppers could improve planetary exploration from both the science and engineering perspectives. Hoppers can travel more quickly than rovers, and they can also cover a greater diversity of terrain. Hoppers could fly over large obstacles and traverse steep inclines, possibly even hopping into or out of craters. They might also provide unique opportunities for science during a hop, such as low-altitude aerial observations or examinations of cliff faces or canyon walls at various heights. For more in-depth analysis of the ways in which hoppers might contribute to planetary exploration objectives, see [2] and [3]. Hoppers have certain advantages from an engineering perspective as well. For a rover, initial landing and travel over the surface involve two dissimilar types of propulsion; by contrast, a hopper can be 19

1 Introduction<br />

The TALARIS (Terrestrial Artificial Lunar And Reduced gravIty Simulator) hopper is a small prototype<br />

flying vehicle designed to serve as an Earth-based testbed <strong>for</strong> guidance, navigation, and control (GNC)<br />

algorithms that will be used to explore lunar and o<strong>the</strong>r planetary surfaces. To date, nearly all robotic<br />

exploration on <strong>the</strong> surface <strong>of</strong> <strong>the</strong> Moon and o<strong>the</strong>r planets has been done by stationary landers or<br />

wheeled rovers. Hoppers would open up new modes <strong>of</strong> exploration with <strong>the</strong>ir alternate <strong>for</strong>m <strong>of</strong><br />

mobility. However, because <strong>the</strong>y are a new technology without <strong>the</strong> long heritage <strong>of</strong> landers and rovers,<br />

<strong>the</strong>re is a greater need <strong>for</strong> testing to reduce <strong>the</strong> risk associated with hoppers. The TALARIS testbed<br />

provides <strong>the</strong> opportunity to develop and mature hopper-based GNC algorithms on Earth, which allows<br />

<strong>for</strong> a more controlled environment and easier human access <strong>for</strong> modifications, upgrades, and repairs if<br />

necessary.<br />

A hop consists <strong>of</strong> three main phases: propulsive ascent, traverse flight, and s<strong>of</strong>t landing. A commanded<br />

maneuver <strong>of</strong> this type has been per<strong>for</strong>med <strong>of</strong>f <strong>the</strong> Earth once, by <strong>the</strong> Surveyor 6 spacecraft on <strong>the</strong><br />

Moon. On November 17, 1967, after Surveyor 6 had been sitting on <strong>the</strong> lunar surface <strong>for</strong> a week, <strong>the</strong><br />

spacecraft’s three liquid-fueled vernier rocket engines were reignited and fired <strong>for</strong> 2.5 s [1]. The control<br />

system was set such that <strong>the</strong> spacecraft would tilt 7° to <strong>the</strong> west upon lift<strong>of</strong>f, and <strong>the</strong> thrust generated<br />

was sufficient to cause <strong>the</strong> spacecraft to rise to an altitude <strong>of</strong> about 3.5 m and to land 2.4 m away from<br />

its starting point. This allowed Surveyor 6 to send back images <strong>of</strong> <strong>the</strong> surface disturbances at its initial<br />

landing site, providing in<strong>for</strong>mation on mechanical properties <strong>of</strong> <strong>the</strong> lunar surface as well as <strong>the</strong> effects <strong>of</strong><br />

firing rocket engines near <strong>the</strong> surface. Fur<strong>the</strong>rmore, <strong>the</strong> displacement <strong>of</strong> <strong>the</strong> spacecraft provided a<br />

baseline <strong>for</strong> stereoscopic viewing and photogrammetric mapping <strong>of</strong> <strong>the</strong> surrounding lunar terrain [1].<br />

However, <strong>the</strong> Surveyor 6 hop is merely <strong>the</strong> tip <strong>of</strong> <strong>the</strong> iceberg in terms <strong>of</strong> <strong>the</strong> potential value that could<br />

be gained from exploring with hoppers.<br />

Hoppers could improve planetary exploration from both <strong>the</strong> science and engineering perspectives.<br />

Hoppers can travel more quickly than rovers, and <strong>the</strong>y can also cover a greater diversity <strong>of</strong> terrain.<br />

Hoppers could fly over large obstacles and traverse steep inclines, possibly even hopping into or out <strong>of</strong><br />

craters. They might also provide unique opportunities <strong>for</strong> science during a hop, such as low-altitude<br />

aerial observations or examinations <strong>of</strong> cliff faces or canyon walls at various heights. For more in-depth<br />

analysis <strong>of</strong> <strong>the</strong> ways in which hoppers might contribute to planetary exploration objectives, see [2] and<br />

[3]. Hoppers have certain advantages from an engineering perspective as well. For a rover, initial landing<br />

and travel over <strong>the</strong> surface involve two dissimilar types <strong>of</strong> propulsion; by contrast, a hopper can be<br />

19

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