exploring venus with robots and airplanes · 2008. 6. 3. · airplanes. geoffrey a. landis venus...
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![Page 1: Exploring Venus with Robots and Airplanes · 2008. 6. 3. · Airplanes. Geoffrey A. Landis Venus RASC study Mission Goal: Exploring Venus from the surface and the atmosphere cool](https://reader033.vdocument.in/reader033/viewer/2022060519/604c9bc3ac954a750f30c268/html5/thumbnails/1.jpg)
Geoffrey A. Landis Venus
Exploring Venus with Robots and
Airplanes
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Geoffrey A. Landis Venus
RASC study
Mission Goal:Exploring Venus from the
surface and the atmosphere
cool upper
atmosphere
hot lower
atmosphere
very hot
surface
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Geoffrey A. Landis Venus
Science mission for Venus Surface Rover
•Characterize the surface at geologically diverse locations
• emplace seismometers to determine the interior structure
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Geoffrey A. Landis Venus
Venus airplane3 foldsWide wing chord version
Venus airplane3 foldsMedium wing chord version
fold line
Aeroshell diameter1.2 meters
Venus Airplane Design Concept Evolution
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Geoffrey A. Landis Venus
Design evolution of
Venus Aircraft
RASC- August 2003
Design concept 2002
RASC final design 2003
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Geoffrey A. Landis Venus
Venus airplane folded into
aeroshell
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Geoffrey A. Landis Venus
Robotic Exploration
Concept:"brains" of the robot stay in the
cool middle atmosphere
Computer stays in cooler middle
atmosphere
Surface robot uses simple high-
temperature electronics
Aerostat vs. airplane trade study
indicates airplane is preferable
Surface exploration robots
controlled by remote computer
Control & computer
system in airplane
Communications satellite
relays to Earth
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Geoffrey A. Landis Venus
Mission animationAnimation is available at:
http://www.grc.nasa.gov/WWW/5000/pep/photo-space/venus-mission-design.htm
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Geoffrey A. Landis Venus
Surface Rover concept
COMM
Rock Abrasion
Arm (Tool)
X-Ray and
Gamma Ray
Cameras
DIPS Power
Supply
35cm Pressure
Vessel
Supporting
Truss Work
Radiators
Drive
Motors
Seismometer Deployment
Wheel Deployment
Parallelogram Concept
Cameras
Un-pressurized
Instruments
(Place Holder)
CAD model by
Shawn Krizan,
NASA LaRC
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Geoffrey A. Landis Venus
Engines with hot-end above Venus Temperature
ASC-1 and ASC-1HSSingle Convertor Operating over 300 hours
Total hours on all convertors: 1257
1123K (900C) hot-end
363K cold-end
38% efficient, 1.3 kg, 102 Hz, ~3.6MPa,
88 W up to 114 W, 2005
Ref. W.
Wong, GRC
>300 hours
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Geoffrey A. Landis Venus
Stirling Radioisotope
Power Converter
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Geoffrey A. Landis Venus
Radioisotope Power: Sterling conversion
21.6 kgMass
23.4%Overall efficiency
1267 WHeat rejected
1740 WHeat input
500CT (sink)
1200 CT (source)
7 250-W GPHS unitsSource
478WPower output
Stirling cycleType
ValueParameter
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Geoffrey A. Landis Venus
Rover close-up
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Geoffrey A. Landis Venus
Stirling Cooler plus
Radioisotope Power
Converter
Sterling cooler design
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Geoffrey A. Landis Venus
Technology Development: Stirling cooler integrated with power system
Sunpower design is coaxial
with heat exchangers
surrounding the Thermal
Buffer Tube
Sunpower convertor
performance is presently equal
to Northrop Grumman
Predicting 65 Wac,8 months development remaining in
SBIR
Design and evaluation for
higher power is part of the
current SBIR
125 Hz.100 Hz.Frequency
5.28 MPa
(765 psia)
3.65 MPa
(530 psia)Pressure
Northrop
GrummanSunpower
Comparison of Northrop
Grumman & Sunpower
Technology
105 W cooling @ 200 ºC
110 Wac electrical output
1740 W input @1200 ºC
500 ºC reject
Venus Duplex
~8 kg (not including couplings)
50 Wac
Northrop Grumman
Sunpower
Ref. G. Wood
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Geoffrey A. Landis Venus
Venus Surface cooling system
Parameter Value
Type Stirling cycle
Stages 1
Heat sink temperature 500 C
Cold temperature 200C
Heat transferred 105.7 W
Heat rejected 344.6 W
Overall coefficient of
performance
37.6%
Mass 1.6 kg
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Geoffrey A. Landis Venus
High temperature motors/actuators
Motor or actuator Max operating
temperature ( C )
status
Baker Hughes GeoThermal 160 commercial
Swagelock pneumatic 200 commercial
Rockwell Scientific SiC 200 development project
NASA Glenn R&T high-
temperature actuator
400
600
prototype goal
research target
NASA Glenn switched-
reluctance motor
540 demonstrated; 8000 RPM, 27 hours
U. Sheffield Linear actuator 800 technology demonstrator:
1 mm throw, 500N force
Venus Surface Robot Technologies:
motors and actuators
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Geoffrey A. Landis Venus
Switched-reluctance motor
capable of operation at 540 C
•Small version of this motor has now been
demonstrated at Honeybee robotics
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Geoffrey A. Landis Venus
Solar airplanes on Earth
Right: Aerovironment
“Pathfinder”
Below: NASA Glenn
solar airplane team
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Geoffrey A. Landis Venus
For More Details:
• Animation is available at:– http://www.grc.nasa.gov/WWW/5000/pep/photo-space/venus-mission-design.htm
• Mission Design:– G. Landis, "Robotic Exploration of the Surface and Atmosphere of Venus," Acta Astronautica,
Vol. 59, 7, 517-580 (October 2006). Paper IAC-04-Q.2.A.08
• Venus Airplane:– G. Landis, C. Lamarre, and A. Colozza, "Venus Atmospheric Exploration by Solar Aircraft," Acta
Astronautica, Vol. 56, No. 8, 750-755 (April 2005). Paper IAC-02-Q.4.2.03
– G. Landis, C. LaMarre and A. Colozza, "Atmospheric Flight on Venus: A Conceptual Design,"
Journal of Spacecraft and Rockets, Vol 40, No. 5, 672-677 (Sept-Oct. 2003).
• Power and cooling systems:– G. Landis and K. Mellott, "Venus Surface Power and Cooling System Design," Acta Astronautica,
Vol 61, No. 11-12, 995-1001 (Dec. 2007). Paper IAC-04-R.2.06
• High-temperature electronics:– P. Neudeck, NASA Glenn Research & Technology 2005, NASA/TM-2006-214096