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Provider of Near Space Solutions
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Tactical Ballooning & Return Vehicles A New Paradigm for Low Cost Near Space Access & Persistence Near Space Corporation Tim Lachenmeier, PE President Low Cost Access to Near Space Conference Boulder, CO April 26-28, 2007
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Background GSSL/NSC History Return Vehicle Milestones PRV Precedents Current Ballooning Paradigm New Tactical Paradigm Why a Tactical Paradigm Draw Your Own Conclusions OVERVIEW
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Origins 1995 - Founded as GSSL Inc 2006 - Became Near Space Corp Specializing In Near Space Platforms & Vehicles: Analysis Design Fabrication Flight Ops Training COMPANY HISTORY
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Experience: Government NASA - Planetary Technology (Venus, Mars, & Titan) NOAA/NCAR - Atmospheric Research USAF – Tactical Balloon Systems & Return Vehicles Commercial Space Prototyping Flight Test Space Inflatables Laboratories Lawrence Livermore Pacific Northwest National MIT-LL JHU-APL COMPANY HISTORY
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Return Vehicle Milestones: 2001 - NASA ARC/NRL - 1 st HA Deployment (Glider) 2002 - NASA ARC/NRL - 1 st HA Deployment (Powered) 2002 - NASA LaRC/AFS - 1 st HA Deployment (Folded) 2003 – NASA LaRC/AFS – Down Select for Mars Scout 07 2004 - NASA JPL/BOEING – Mars Guided Parachutes 2005 - USAF Tactical Balloon/Return Vehicle 2006 – NASA LaRC/AFS – Down Select for Mars Scout 11 35 High Altitude Deployment Tests >100,000 ft COMPANY HISTORY
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Return Vehicle Video 35 High Altitude Deployment Tests >100,000 ft PRV PRECEDENTS First Video
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CURRENT BALLOON PARADIGM Current Paradigm Built on 50+ Years of Success Commonly Referred to as “Scientific Ballooning”
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DOD Discovers Tactical Ballooning PARADIGM CHANGE
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DOD Discovers Tactical Ballooning PARADIGM CHANGE
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Traditional Launch What Is The New Paradigm? Tactical Balloons Return Vehicles Tactical Launch
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PAST PROBLEMS What’s Wrong With The Old Paradigm? Ground Winds > 5 Knots Logistics Inflation/Launch Infrastructure Payload Recovery Cost
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PROBLEM #1: GROUND WINDS > 5 KNOTS Ground Wind Problem Linked to Inflation and Launching At Low Altitude: Relatively Small Gas Bubble Excess Material Material Becomes Large Sail High Potential for Film Damage At High Altitude: Gas Expands Material is Fully Deployed Balloon Moves with the Wind Low Potential for Film Damage
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General Approach: View Wind as the Enemy Common Approach: Enclose Balloon in a Protective Bag Before Launch Prevents Balloon Damage from Ground Contact PROBLEM #1: GROUND WINDS > 5 KNOTS
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NSC Developed a Tactical Launch Bag* Wind Inflates Bag Orients Like a Wind Sock Creates a Still-Air Environment for Balloon Inflation NSC SOLUTION TO PROBLEM #1 * Patent Pending
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Instead of Launching a Deployed Main Balloon, NSC Developed a Tandem Balloon System* NSC SOLUTION TO PROBLEM #1 * Patent Pending
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NSC SOLUTION TO PROBLEM #1 Traditional Launch Tactical Balloon System Small Tow Balloon & Packed Main Allows Launch from Ships, Parking Lots, Small Clearings Tactical Launch
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TACTICAL PARADIGM Tactical Launch Second Video
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One or Two People Can Now Set Up & Launch Large Balloons! Proven in 26+ Knot Winds! Tactical Launch Bag Tandem Balloon System NSC SOLUTION TO PROBLEM #1
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PROBLEM #2: LOGISTICS Traditional Balloons Require Significant Support People Equipment Inventory
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NSC SOLUTION TO PROBLEM #2 Tactical Launch Bag & Tactical Balloon System Allow One or Two People to Launch Balloons Minimizes Logistics Footprint
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Mission Flexibility Requires Large Inventory of Standard Balloons Balloons Sized by Payload & Altitude PROBLEM #2: LOGISTICS
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Inventory of Adjustable Tactical Balloons Allows Flexibility Eliminates Custom Manufacturing NSC SOLUTION TO PROBLEM #2
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More Launch Opportunities - Fewer Resources! Tandem Balloon System Inventory of Adjustable Balloons Tactical Launch Bag NSC SOLUTION TO PROBLEM #2
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PROBLEM #3: INFLATION INFRASTRUCTURE Traditional Inflation Requires: Numerous People Ground Anchor Continuous Monitoring Ground Wind < 5 Kts
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Tactical Launch Bag & Tactical Balloon System Enables One Person Inflation in Wind > 30 Kts NSC SOLUTION TO PROBLEM #3
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Autonomous Inflation* Simplifies Inflation Process Skilled Operator Not Required Continuous Monitoring Not Required “Gasoline Pump” Hook Up Turn One Valve & Walk Away Gas Supply Turns Off Automatically When Required Amount Delivered NSC SOLUTION TO PROBLEM #3 * Patent Pending
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More Frequent Streamlined Launches! Tandem Balloon System Autonomous Inflation Tactical Launch Bag NSC SOLUTION TO PROBLEM #3
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PROBLEM #4: PAYLOAD RECOVERY Current Payload Recovery Usually by Parachute Limited Trajectory Control Very Small Achievable Cross Track Distances Chase & Recovery To Uncontrolled Areas Required Other Option: Self-Destruction at Mission Termination Wastes Valuable Payloads
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More Efficient Solution: Embed Payload in a Payload Return Vehicle* Returns Payload Significant Distances Crosswind, Upwind & Loitering Capable Standardized Interface Makes Payload Swap-Out Simple Multiple Missions, One Platform NSC SOLUTION TO PROBLEM #4 * Patent Pending
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More Flights, Fewer Resources, Same Payload! Payload Return Vehicle NSC SOLUTION TO PROBLEM #4
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PROBLEM #5: COST Wind Delays = $ People, Equipment & Inventory = $ Parachute Recovery/ Destruction = $
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NSC SOLUTION TO PROBLEM #5 Lower Cost Alternative! Eliminates Wind Delays Less People, Equipment & Inventory Same Payload, Multiple Flights
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Primary Application Payload < 200 lbs Altitude < 100,000 ft Duration < 48 hrs Near Space Corporation NOT FOR EVERYONE!
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Tactical Ballooning & Return Vehicles A New Paradigm for Low Cost Near Space Access & Persistence Near Space Corporation Tim Lachenmeier, PE President Questions?
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POC : Tim Lachenmeier Email: Tim.Lachenmeier@nsc.aero Phone: (503) 842-1990 Fax: (503) 842-1923 Web Site: www.nsc.aero Provider of Near Space Solutions
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