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TFAWSMSFC ∙ 2017
Presented By
Ron Creel
Retired Apollo Lunar Roving Vehicle
Team Member
Interactive LUROVA™ Thermal Model
for the STEM Simulation Game
Thermal & Fluids Analysis Workshop
TFAWS 2017
August 21-25, 2017
NASA Marshall Space Flight Center
Huntsville, AL
TFAWS Interdisciplinary Paper Session
TFAWS 2017 – August 21-25, 2017 2
Outline
• Apollo Lunar Rover Thermal Modeling for Mission Support
• LUROVA™ Thermal Modeling for TFAWS
• LUROVA™ Simulation Game for STEM
• Interactive LUROVA™ Simulation Game Thermal Model
• Verification / Correlation of the LUROVA™ Sim Game Model
• Future Plans for the LUROVA™ Simulation Game
• LUROVA™ Poster and Demonstration for Attendees
• Test Correlated Thermal Models Were Vital for Rover Success
TFAWS 2017 – August 21-25, 2017 3
Apollo Lunar Rover Thermal Testing / Modeling
Clean αS= 0.07
Qualification and Flight Units TVAC
Ron Creel with Rover Mobility TVAC Test Unit
181 Node SINDA Thermal Model for Apollo 15
Folded Rover Modeled, but not Tested
Transportation Phase
3 Rev/Hour Rotation
19 Node Forward Chassis Thermal Model for Apollo 16 and 17
Astronaut
Silver Snoopy
Awarded for
Thermal Modeling
after Apollo 16
in July, 1972
2590 Conductors
128 Heating Arrays
• LUnar ROVing Adventures - LUROVA™ for Apollo 15, 16, 17
TFAWS 2017 – August 21-25, 2017 4
LUROVA™ Simulation for Apollo Mission Support
19 Node Thermal Model Input
(Replaced Cumbersome and Slow
181 Node Model)
Astronauts Appreciated Timely and Accurate
Thermal Modeling
20 Meter Resolution Terrain DataRon at LUROVA™ Thermal Model Control Console
Dust Coverage Degradation Effects Modeled
• 2006 – Presented Apollo Lunar Roving Vehicle mission performance and lessons
learned, and introduced Rover mission support thermal models
– Thermal models originally planned for CD to accompany retrospective book
– 19 Node model then used for NASA Nightrover Power Storage Challenge
• 2014 – 181 node SINDA thermal model updated with render engine provided
external surfaces for radiation conductors and solar heating
– Conductors and solar heating needed to add to
historical SINDA model nodes listing
– 911,509 poster polygons reduced to 7805 polygons
for TRASYS surface modeling
• 2017 – LUROVA™ thermal model incorporated in a
Science, Technology, Engineering, and Mathematics (STEM) simulation
game for interactive student challenge and Moon exploration experience
– Trademark purchased for LUROVA™ Simulation Game
– Initial game structure contributed by Computer Science associate professor and
students at the University of Alabama in Huntsville (UAH)
– Exploration realism is improved by interactive use of actual lunar terrain data
collected since 2009 by NASA Lunar Reconnaissance Orbiter (LRO) spacecraft
TFAWS 2017 – August 21-25, 2017 5
LUROVA™ Thermal Modeling for TFAWS
• “Simulation Game = Attempt to copy various activities from real life in
the form of a game for education, training, analysis, or prediction.”
TFAWS 2017 – August 21-25, 2017 6
LUROVA™ Simulation Game for STEM
LUROVA™ STEM Simulation Game Provides Apollo Mission Support Thermal Model with
High Resolution Surface Model and LRO Terrain Data
Variable Planning and Preparation for MissionTiming, Location, and Rover ConfigurationHand Controller for Driving and Steering Battery Power Usage and Solar Heating
Component Failures and Cooldown Dust Effects
LRO
Lunar Reconnaissance Orbiter (LRO) Collecting
0.5 Meter Resolution Terrain Data Since 2009
TFAWS 2017 – August 21-25, 2017 7
Interactive LUROVA™ Simulation Game Play
Adventurer Deploys Rover
from Lunar Module (LM)
and Loads Equipment
Adventurer Drives Rover
to Pre-planned Station
Stops for Exploration
and Sample Collections
• Adventurer Plans and Executes Exploration Traverses, and Views:
- Computed Position, Heading, Speed, Slope, Power, and Temperature Results
Adventurer Activates Rover
Switches and Uses Hand
Controller for DrivingAdventurer Views Heading, Speed, and Temperatures
TFAWS 2017 – August 21-25, 2017 8
Interactive LUROVA™ Sim Game Thermal Model
• Simulation Game Thermal Model Increases STEM Exploration Realism – SINDA Provides Responsive Thermal Programming
SINDA Model - 181 Nodes
“Operations” Logic,
Solar Heating Calls in
“Variables 0”, and
Subroutines for Sun Angles,
Moon Temp,
Internal/External Heating,
Wax Melt Status
[ALP = Radiator Solar Absorptance for Separate COOLDOWN.EXE]
• Simulated Operation During Driving & Cooldown Periods Verified
Verification of the LUROVA™ Sim Game ModelTe
mp
erat
ure
–D
eg. F
Driving10 kph,
2 deg Slope
Driving10 kph,
4 deg Slope
Driving10 kph,
2 deg Slope
StoppedCovers Closed
StoppedCovers
Opened
StoppedCovers
Opened
BatterySurvival Limit
BatteryOperating Limit
Battery 1
Battery 1
Battery 2
SPU Wax Melting
DCE Wax Melting
DCE
SPU
DGU SPU + Wax
Battery 2 DCE + Wax
LUROVA™ Thermal Model - Driving and Cooldown Verification
Tem
per
atu
re –
Deg
. F
Time – Hours
Radiator Solar Absorptance = 0.35
Apollo 16 EVA 1Forward Chassis Electronics
Tem
per
atu
re –
Deg
. F
Time – Hours
Time – Hours
Front Mobility
Rear Mobility
Lunar Rover Batteries Supplying Navigation and LCRU Power
Right SideLeft Side
Right SideLeft Side
Heading = 0.0 Deg
Heading = 0.0 Deg
TFAWS 2017 – August 21-25, 2017
2 3
4
51
1
2
3 5
4 6
4 6
Driving
Cooldown
9
Apollo Dust Brush
• LUROVA™ Simulation Game Correlates Well With Last Rover Sortie
– Lunar Dust Degradation Effects on Radiators Studied
Correlation of the LUROVA™ Sim Game Model
TFAWS 2017 – August 21-25, 2017
Tem
per
atu
re –
Deg
. F
Astronaut Brushing
Dust from Radiator
Tem
per
atu
re –
Deg
. F
Time – Hours
Right Battery No. 2
Left Battery No. 1
Clean αS = 0.07
αS = 0.15
αS
X
XX
X
Cooldown after Apollo 16 EVA 2
Best Match
Dust Degradation of Radiator Solar Absorptance -
X
X
X
10
• Finish Interactive LUROVA™ STEM Simulation Game Development– Opportunities for Student “Beta Testing” and Expansion for VR, “MAROVA”
11
Future Plans for the LUROVA™ Simulation Game
TFAWS 2017 – August 21-25, 2017
TFAWS 2017 – August 21-25, 2017 12
LUROVA™ Poster and Demonstration for Attendees