student ballooning and the high altitude student platform · • provide students with real-world...
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Student Ballooning and theHigh Altitude Student Platform
T.G. Guzik and J. P. WefelLouisiana Space Consortium,
L i i St t U i it B t R LA U S ALSU 10/19/09 NSG Directors Meeting - Oct 23, 09 1
Louisiana State University, Baton Rouge, LA U.S.A.
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HASP focuses on university students
• Operates as a partnership between the NASA Balloon Program Office (BPO) and Louisiana Space Consortium (LaSPACE)Office (BPO) and Louisiana Space Consortium (LaSPACE)– BPO provides balloon, launch and flight services– LaSPACE maintains HASP & supports the student payloads
• Provide students with an annual near-space flight opportunity• Support payloads that perform technology testing or scientific
measurement• Opportunity to test fly prototype student satellite components• Provide students with real-world science / engineering project
development experiencesdevelopment experiences• Keep students excited about a science, technology or engineering
career
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Major HASP Features
• Support 12 student built payloads– Eight small payloads < 3 kgg p y g– Four large payloads < 20 kg
• Fly to an altitude > 36 km for a duration of ~20 hoursduration of ~20 hours
• Standard interface for each payload– Mechanical plate interface
S i l d li k l 4800 b– Serial downlink telemetry < 4800 bps– Serial uplink commands– Discrete commanding – 32 VDC power @ < 2.5 Amps– Analog (0 to 5 VDC) downlink– Downlink available in near real time
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• Include CosmoCam for real time video during launch & flight
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Typical Payload Development Schedule
• Application process takes place in the fall– Release of CFP (Call for Payloads): October 1
• Payload development takes place in the spring
( y )– Applications due: December 18– Selection announcement: mid-January
• Payload development takes place in the spring– Require monthly status reports and telecon meetings– Preliminary thermal / vacuum test the 3rd week of May
• Integration occurs during 1st week of August– Use the Columbia Scientific Balloon Facility (CSBF)
in Palestine, Texas– Must pass a thermal / vacuum test to be flight certified
• Flight Ops take place around Labor Day– Use the CSBF balloon launch facility in Ft Sumner
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Use the CSBF balloon launch facility in Ft. Sumner, New Mexico
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Typical HASP Flight
• HASP is a medium weight payload– Total suspended weight is 2,000 pounds
• Usually launch just after dawnR i d l l l d hi h l i d
p g , p– Use a 11 million ft3 zero pressure balloon
– Require ground, low level and high altitude winds to cooperate
• Flight lasts about 17 hoursHASP launch at 8 times normal
speedFlight lasts about 17 hours– Takes about 2 hours to get to ~36 km (~120,000 feet)– Take about 45 minutes to come down on parachute
Get a day and some night in “space”
speed
– Get a day and some night in space
• HASP has now flown four times– Total time at float is more than 75 hours
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– Expect to continue flights each year
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HASP 2006 & 2007 Flights
2006
2007
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HASP 2008 & 2009 Flights
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Alaska
HASP Activities Status as of July 2009
W hi t
Maine
New Hampshire
Vermont
Washington
Oregon Idaho
Montana
Wyoming
NorthDakota
SouthDakota
MinnesotaWisconsin
Michigan
New York
PennsylvaniaNew
Jersey
Hampshire
Massachusetts
Rhode IslandConnecticut
32
1
California
NevadaUtah
Colorado
Nebraska
Kansas Missouri
IowaIllinois
Kentucky
IndianaOhio
WestVirginia
Virginia
Maryland
Washington DC
Delaware
N th
2
32
4
ArizonaNew
Mexico
HawaiiOklahoma Arkansas
Mississippi
Alabama
TennesseeNorth
CarolinaSouth
Carolina
Georgia7
11
Texas LouisianaFlorida
States Utilized HASP (11)States have Not Utilized HASP (39+DC)
College/University payloads1
4
11
2
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Slide courtesy of NASA BPO – M. Said
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HASP has involved many students from across the countrythe country
• 44 student payloads have been accepted for flight since 20062006– 8 flown on HASP 2006– 11 selected (10 flown) for HASP 2007( )– 13 selected (10 flown) for HASP 2008– 12 selected (6 flown) for HASP 2009
• Greater than 70% success during 2006, 2007 & 2008• A total of 191 students have been involved with HASP
25 i 2006 70 i 2007 96 i 2008– 25 in 2006, 70 in 2007, 96 in 2008• Participants from 17 institutions across 11 states• Payloads cover a broad range of subjects
LSU 10/19/09 NSG Directors Meeting - Oct 23, 09 9
• Payloads cover a broad range of subjects
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Examples of flown payloads• Louisiana State University – Baton Rouge (2006, 2007): Study
the flow characteristics of various rocket nozzles as a function of altitudealtitude
• Montana State University (2007, 2008, 2009): Passive high altitude particle capture experiment
• West Virginia University (2007): High altitude cosmic ray d t tdetector
• Virginia Polytechnic Institute & State University (2007, 2008): Prototype for a Lunar magnetic field instrument, (2009): Flying InfraRed Experiment for Lunar Investigation (FIREFLI)
• University of Alabama – Huntsville (2006, 2007, 2008): Infrared imaging of the balloon thermal characteristics
• University of Colorado (2008, 2009): Assessment of astronomical observations from balloonsastronomical observations from balloons
• University of Maryland (2008, 2009): Flight test of compact radio telemetry system
• University of North Dakota / University of North Florida (2008 2009): De elopment and test of a micro scale o one
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(2008, 2009): Development and test of a micro scale ozone detector – Resulted in publication and Masters Thesis
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Montana Particle Capture Experiment
• Experiment to capture cosmic particles and analyze their morphology and composition in the laboratory
– Trap particles on optically clear plates coated with silicone oil– Flew in 2007 (success), 2008 (not so good) and 2009 (looks
good so far)• Light scattering particle detector to examine vertical
distribution of >1μm size dust particlesh i f h d i i l– Test homogeneity of stratosphere during particle capture
– New for 2009Opening of MSU experiment
(8 times normal speed)
Flow
He/Ne laser
Flow
Light trap
pump
laser
detector
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Images courtesy MSU teampump
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Particle Capture Preliminary Results
Laser Particle Counters Cosmic Dust Capture Box
• Analysis of 2007 data has examined 400• Both particle counters gave similar
readings – ground – 36,000 feet. • Uncertain as to why the measurements
• Analysis of 2007 data has examined 400 particles so far
• HASP 2009 capture plates exposed for 12-hours and the optical analysis of the plates
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ydiverged after that. has started
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Found Different Types of Particles
RocketExhaustExhaust
VolcanicVolcanicDust ?
CosmicDust ?
LabC t i t
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Contaminant
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North Dakota / North Florida Prototype ITO Ozone sensorsPrototype ITO Ozone sensors
• Collaboration between two universities in two states– University of North Florida (sensor development)– University of North Dakota (payload development)University of North Dakota (payload development)
• Flight test of prototype solid state gas-sensitive resistor sensor– CMOS indium tin oxide (ITO) sensor– Material doped in order to be sensitive to different gases
• Payload has successfully flown twice• Payload has successfully flown twice– Array of 24 Ozone sensors of three different types in 2008– Array of Ozone and NOX sensors in 2009
Single ITO Sensor ITO Sensor Surface 24 Sensor Flight ArraySingle ITO Sensor ITO Sensor Surface 24 Sensor Flight Array
1 μm
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ITO Sensors Flight Results
• The electrical resistance of ITO increases in the presence of oxidizing gases
V it i fill d b h ti l lSensor Calibration
– Vacancy site is filled by a charge accepting molecule– Electrons are depleted from conduction band, leading to
an increase in resistance• Sensors were calibrated with known O3 concentrations• HASP 2008 flight results yield a measured ozone• HASP 2008 flight results yield a measured ozone
profile very similar to what was expected.• Project has already resulted in one publication and one
Master’s Degree thesis.
Expected Ozone Concentration
HASP 2008 Flight Result
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Balloon Observatory for Wavelength and Spectral Emission Readings (BOWSER)Spectral Emission Readings (BOWSER)
• University of Colorado (Boulder) team experiment is design to test the feasibility of balloon-borne observatories
U f LED t k b i ht i th– Use an array of LED sensors to measure sky brightness in the visible, ultraviolet and infrared
– Use wide and narrow field cameras to image star fields and celestial objects
– Include a magnetometer compass, accelerometers and gyroscopes g p , gy pto determine the platform attitude and stability during the flight
• Flown in 2008 (DIEHARD) and 2009 (BOWSER)
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BOWSER Imaging of Venus
Images courtesy UC team
Imaging VenusExposure time:Exposure time:
1/13 second
Simulated Image
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BOWSER Imaging of Big Dipper Stars
Exposure time:1 second
Simulated Image
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Call for Payloads 2010
CFP document and application materials is available on the “Participant Info” tab of the
HASP b iHASP websitehttp://laspace.lsu.edu/hasp/Participantinfo.html
Q&A Teleconference November 13, 2009 at 10 am (central time)
Dial 1 866 717 2684 ID 6879021Dial 1-866-717-2684, ID 6879021
Completed applications are due on December 18, 2009
LSU 10/19/09 NSG Directors Meeting - Oct 23, 09 19
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Submission Instructions• E-mail PDF version of application by 11:59 pm (central time) to
[email protected] @p p y• Mail hardcopy of application to
T. Gregory Guzik202 Nicholson Hall / Tower Drive202 Nicholson Hall / Tower Drive
Department of Physics & AstronomyLouisiana State University
Baton Rouge, LA 70803-4001g ,• Applications will be reviewed by HASP Management at LSU
and the NASA Balloon Program Office– Applications will be reviewed for completeness consistency scientific orApplications will be reviewed for completeness, consistency, scientific or
technical justification, and ability to fit within the HASP constraints– Priority will be given to payloads that are clearly designed, built, managed
and operated by students
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• Decisions will be announced by January 15, 2010