PLANETARY PROBE DESIGN WORKSHOP: COLLABORATIVE HANDS-ON SMALL SATELLITE TRAINING FOR ENGINEERING STUDENTS
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1 PLANETARY PROBE DESIGN WORKSHOP: COLLABORATIVE HANDS-ON SMALL SATELLITE TRAINING FOR ENGINEERING STUDENTS Georg Herdrich (1, 2), René Laufer (2,1), Adam S. Pagan (1) (1) Institute of Space Systems, University of Stuttgart, Germany, (2) CASPER, Baylor University, Waco, Texas, USA April 2015, Berlin, Germany INSTITUT FÜR RAUMFAHRTSYSTEME
2 Motivation Adapt to changes in university-level engineering education Hands-on projects on undergraduate and graduate level Offering research experience for undergraduates in addition to theses Building on the institute s existing, positive experience with workshop format (graduate/post-graduate level) in a concurrent design environment Using CubeSat nano satellite format as a proven tool for education Platform to perform research in dedicated fields (e.g. atmospheric entry, electric propulsion) Student small satellite projects as a supplement - not a replacement to the institute s academic small satellite research program Using low-cost and fast-schedule opportunities for sub-projects within the overall format to provide sense of achievement Applying Do One Thing Well (mission complexity) and Virtual Exploration is NOT an Option (hands-on) approach
3 Student Involvement The Planetary Probe Design Workshop provides an educational framework for additional surrounding activities. Annual iteration of the one week Planetary Probe Design Workshop since 2012 with increasing number of participants international and from various years of study. Numerous student theses and project/internship work Student small satellite interest group KSat e.v.: Currently >25 highly motivated active members and growing! KSat Team (beginning of 2015)
4 1 st PPDW Project: CAPE Mission IRS faculty & staff PhDs (TPS/SEP) Visiting experts External theses 1 Deployment e.g. from ISS 3 Separation PPDW phase 0/A reports DLR Rexus 19/20 participation Bachelor theses on CAPE 2 De-orbit De-orbit down to separation altitude Atmospheric measurements PPT demonstration at 125 to 150 km altitude 5 Transfer of re-entry data via satellite Transmission of data through Iridium network 4 Re-entry of MIRKA2 Measurement of the ambient conditions and the re-entry performance of the capsule 6 Demise of SDM, impact of capsule Potential for monitoring of break-up and demise
5 MIRKA2-RX Mission (PDR passed 12/2014) T=26s: burn-out REXUS sounding rocket T=140s: apogee at km Ejection MIRKA2-RX Mirror System MIRKA2-RX Capsule Deutschland T=0s: launch (ESA 2007) T=~800s
6 IRS (G. Herdrich) Management and lead, System Design Thermochemistry, Instrum. DLR Stuttgart (H. Hald) Integration of capsule NASA Goddard (J. Esper) Potential flight opportunity Space Science Lab (R. Laufer, CASPER, Baylor University) Systems Engineering Support Small Satellite Design KSat IRS Student team Gradel (D. Petkow) University of Adelaide (M. Kim) Blackout assessment ISA (Ph. Reynier) Assessment of laminar/ turbulent transition Trajectory simulation ÖWF (N. Frischauf) International outreach CE (R. Gabrielli) National outreach and regulations (CE) ASA (M. Auweter-Kurtz) System and mission analysis support OHB Sweden (A. Demairé) PPU for deorbit electric propulsion Thales Alenia Space Deutschland Modelling + simulation of capsule's dynamic motion during initial reentry phase Facilities and logistical support of student activities
7 Summary and Outlook PPDW is an educational element in (especially) undergraduate aerospace engineering education offering an intense, mission-focused, goal-oriented workshop-type course utilizing a concurrent design environment Utilizing highly cost-effective CubeSat standard as a platform for education, science and engineering research Enables highly motivating, inspiring and challenging types of missions Network of partners provide opportunities for students PPDW 2016 in the March/April 2016 timeframe Possible growth into two workshops per year (spring & fall) Like to know more? Contact Georg Herdrich ([email protected]) or Rene Laufer ([email protected])
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