dc.contributor.author |
Badescu, Mircea |
|
dc.contributor.author |
Backes, Paul |
|
dc.contributor.author |
Moreland, Scott |
|
dc.contributor.author |
Okamoto, Tyler |
|
dc.contributor.author |
Riccobono, Dario |
|
dc.contributor.author |
Kugel, Matthias |
|
dc.contributor.author |
Brinkman, Alex |
|
dc.contributor.author |
Choukroun, Mathieu |
|
dc.contributor.author |
Molaro, Jamie |
|
dc.contributor.author |
Newbold, Timothy |
|
dc.contributor.author |
Heness, Andrew B. |
|
dc.date.accessioned |
2022-04-12T00:02:30Z |
|
dc.date.available |
2022-04-12T00:02:30Z |
|
dc.date.issued |
2021-03-06 |
|
dc.identifier.citation |
2021 IEEE Aerospace Conference, Big Sky, Montana, March 6-13, 2021 |
|
dc.identifier.clearanceno |
CL#21-1204 |
|
dc.identifier.uri |
http://hdl.handle.net/2014/54578 |
|
dc.description.abstract |
The novel Dual-Rasp sampling system has been developed for landed missions to low gravity planetary bodies and is particularly well suited for the unique environment of Saturn’s moon Enceladus. The Dual-Rasp sampling system has two counter-rotating rasp cutters that remove material from the surface and direct it into a guide. The cuttings follow the guide into a sample collection cup. When the sampling collection completes, the tool reconfigures by rotating the guide to create a closed circuit for pneumatic sample transfer from the collection cup to science instruments on the lander. A valve opens a gas tank and the gas flows from that tank into the sample collection cup and down rigid tubing to the science instruments chamber on the lander. A two degree of freedom arm with base actuators is used to deploy the sampler and control its sampling location. |
|
dc.description.sponsorship |
NASA/JPL |
en_US |
dc.language.iso |
en_US |
|
dc.publisher |
Pasadena, CA: Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2021 |
|
dc.title |
The Dual-Rasp Sampling System Design with Closed Pneumatic Sample Transfer |
|
dc.type |
Preprint |
|