Note: “space drives” refers to transmissions including gears or
rollers, bearings, lubricants, seals, etc. used on spacecraft or planetary
exploration vehicles.
| Name / Job function
Address Phone / Email |
____________________________________________________________
____________________________________________________________ ____________________________________________________________ |
| Area(s) of concern | Manned spacecraft | ____________ | Unmanned spacecraft | ____________ |
| Planetary vehicles | ____________ | Other | ____________ |
Please rate technology needs on a 0-4 scale. (Rate only those
in your area of expertise.)
0=no need, 1=minor, 2=average, 3=major, 4=critical
I. General Drive Characteristics
Rating of Needs
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| 1.) High power capacity | ________ | ________ | ________ | ________ |
| 2.) Design guidelines | ________ | ________ | ________ | ________ |
| 3.) Fail safe/redundant design | ________ | ________ | ________ | ________ |
| 4.) Overload capacity | ________ | ________ | ________ | ________ |
| 5.) Mechanical efficiency | ________ | ________ | ________ | ________ |
| 6.) Wear | ________ | ________ | ________ | ________ |
| 7.) Long-life solid lubricants | ________ | ________ | ________ | ________ |
| 8.) Replenishing solid lubricants | ________ | ________ | ________ | ________ |
| 9.) Developing liquid/grease lube systems | ________ | ________ | ________ | ________ |
| 10.) Liquid / grease lubricants | ________ | ________ | ________ | ________ |
| 11.) Lubricant outgassing | ________ | ________ | ________ | ________ |
| 12.) Robustness to (hot or cold) temperatures | ________ | ________ | ________ | ________ |
| 13.) Robustness to thermal cycling | ________ | ________ | ________ | ________ |
| 14.) Robustness to chemical degradation | ________ | ________ | ________ | ________ |
| 15.) Tolerance to dust/wear particles | ________ | ________ | ________ | ________ |
| 16.) Sealing out dust/contaminants | ________ | ________ | ________ | ________ |
| 17.) Sealing in lubricants | ________ | ________ | ________ | ________ |
| 18.) Tolerance to radiation | ________ | ________ | ________ | ________ |
| 19.) Lightweight designs for short life mission | ________ | ________ | ________ | ________ |
| 20.) Other(s) | ________ | ________ | ________ | ________ |
0=no need, 1=minor, 2=average, 3=major, 4=critical
II. What are technology needs for various size / power
levels and rotation speeds?
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| 1.) Micro/nano machines | ________ | ________ | ________ | ________ |
| 2.) Small robot machines (Pathfinder) | ________ | ________ | ________ | ________ |
| 3.) Medium size rovers (Apollo Moon rover) | ________ | ________ | ________ | ________ |
| 4.) Large rovers ("Winnebago") | ________ | ________ | ________ | ________ |
| 5.) High-power machines (mining equip.) | ________ | ________ | ________ | ________ |
| 6.) Very slow/intermittent speed (stiction) | ________ | ________ | ________ | ________ |
| 7.) Slow speed (10-200 rpm) | ________ | ________ | ________ | ________ |
| 8.) Medium speed (200-2,000 rpm) | ________ | ________ | ________ | ________ |
| 9.) High speed (> 2,000 rpm) | ________ | ________ | ________ | ________ |
0=no need, 1=minor, 2=average, 3=major, 4=critical
III. Where are there needs for development of drive
concepts?
| Manned | Unmanned | Planetary | Other | |
| 1.) Conventional single/compound gear meshes | ________ | ________ | ________ | ________ |
| 2.) Epicyclic (planetary) systems | ________ | ________ | ________ | ________ |
| 3.) Worm/wheel drives | ________ | ________ | ________ | ________ |
| 4.) Traction drives | ________ | ________ | ________ | ________ |
| 5.) Harmonic drives | ________ | ________ | ________ | ________ |
| 6.) Non-conventional | ________ | ________ | ________ | ________ |
| 7.) Other | ________ | ________ | ________ | ________ |
IV. What technology problems do you anticipate for future space
drives?
V. Are you interested in collaboration with Glenn Research Center in a space drive systems technology development program?
Y / N
Please return survey to fred.Oswald@grc.nasa.gov, fax to 216 433-3954 or mail to
Mechanical Components Br. MS 23-3, NASA Glenn Research Center, Cleve, OH 44135rev 15 Nov 00