NASA/GSFC’s Wallops Flight Facility Facility Overview John H. Campbell Director Wallops Flight Facility On the Coast! You are here!
Download ReportTranscript NASA/GSFC’s Wallops Flight Facility Facility Overview John H. Campbell Director Wallops Flight Facility On the Coast! You are here!
NASA/GSFC’s Wallops Flight Facility Facility Overview John H. Campbell Director Wallops Flight Facility On the Coast! You are here! Wallops History •Established by National Advisory Committee for Aeronautics (NACA) in 1945 under Langley as a flight test site for aerodynamic research •1945-1958: •1958-1974: •1974-1981: •1981: Pilotless Aircraft Research Station Wallops Station Wallops Flight Center (independent) Wallops Flight Facility (under GSFC) •Over 16,000 launches conducted during 60 year history •Wallops mission has evolved to include: •Flight program management •Technology development •Scientific research The Wallops Mission Vision Wallops Flight Facility will be a national resource for enabling low-cost aerospace-based science and technology research Mission •Enable scientific research •Development/deployment of suborbital & small orbital carriers •Earth science research •Mission services •Enable frequent, safe, and low-cost access to space •Advanced technology development, •Testing & operational support •Facilitation of the commercial launch industry •Provide science and technology educational opportunities, and pursue innovative partnerships with academia, other government agencies, and industry Wallops Flight Facility Three Land Areas •Wallops Main Base 6000 Acres 1900 Acres •Administrative & Technical Offices •Tracking & Data Acquisition •Range Control Center •Ordnance Storage/Processing •R&D, Processing Facilities •Research Airport •Navy Administration/Housing •Coast Guard Housing •Wallops Island 3000 Acres •Launch Sites •Blockhouses •Radar •Processing Facilities •Dynamic Spin Balance •Navy Operational Facilities •Wallops Mainland 100 Acres •Tracking & Data Acquisition •Marshland 1000 Acres Wallops Main Base Wallops Island Other Wallops Organizations Navy/Surface Combat Systems Center Mid-Atlantic Regional Spaceport Naval Air Warfare Center (Patuxent River) National Oceanic and Atmospheric Administration U. S. Coast Guard Marine Science Consortium Wallops Workforce NASA, Navy, NOAA NASA Workforce Total=1174 260 Civil Service Contractors Wallops Employment Total=1777 914 NASA Navy NOAA 98 515 1174 NASA/Wallops Research Carriers Sounding Rockets •20-35 missions per year •Science/technology experiments •World-wide launch locations •Spacecraft built & tested in-house Scientific Aircraft •Atmospheric science research •Flying laboratories •In-house aircraft mods. •Worldwide mission support Scientific Balloons • •20-35 missions per year •Worldwide mission support •Technology plans include 100+ day missions & trajectory control Unpiloted Aerial Vehicles •Earth science research •Brokering services •New technology developments Small Orbital Payload Carriers •Description: •Development of small orbital payload carriers to support NASA science, technology, & educational payloads • •Previous Programs: •Shuttle Small Payloads (Get-Away Special, Hitchiker) •UNEX/UnEss (e.g., CHIPS) •Current Initiative: •Low-cost, multiple payload ejector (MPE), compatible with a range of small payload designs • •Designed for use with NASA/DARPA Falcon-class ELVs •Proto-flight unit to be completed by Fall 2006 •1st flight expected in 2008 Multi-Payload Ejector (MPE) Multi-Payload Ejector (MPE) •Offers opportunity for responsive, low-cost small science, technology, and educational satellites •Supported payload classes •Primary (1): Up to 400 lbs. •Secondary (up to 6): ~100 lbs. each •Tertiary (up to 12):~2 lbs. each (“Cubesats”) •Design characteristics: •Low-recurring cost (<$1.5M) •Producible in <6 months •Modular design with very limited mission-unique engineering •In-house design/development by NASA & contractor team Wallops Launch Range Missions •Suborbital & orbital science rockets •Launch vehicle R&D testing •Educational flight projects •Targets & training Hybrid Rocket Test Flight •Supports •NASA •DoD •Commercial launch industry •Full suite of support services Vandal Target •Launchers •Processing facilities & logistics •Range safety •Tracking & data services •Focus on R&D missions •Dynamic science events •Developmental vehicles Talos Aries Pegasus ELV Wallops Launch Sites Pad 0A Pad 0B Pad 1 Pad 2 Pad 3A Pad 3B Pad 4 Pad 5 “Conestoga” Launch Complex (MARS) Universal ELV Launch Complex (MARS) 50K “Starbird” rail launcher 20K ARC rail launcher 7.5K MRL rail launcher Scout launcher (Inactive) Navy Talos Launcher (Vandal/Coyote) Navy BQM Target launch site Inactive Pad 20K AML Launcher 20K ARC Rail Launcher 50K Rail Launcher MARS “Conestoga” Launch Complex MARS Universal Launch Complex Wallops Research Airport •Primary Missions: Water Ingestion Testing •Aircraft & airport research •Basing for WFF Earth Science & transient research aircraft •Support to WFF Launch Range •Runways 04/22: 8750’ x 150’ 10/28: 8000’ x 200’ 17/35: 4820’ x 150’ + Island UAV Runway •Research Examples Aircraft Noise Testing •UAV operations •Aircraft & airport safety testing •Aircraft noise measurement •Landing system instrumentation demonstration •Features Wake Vortex Studies •Low-traffic •Restricted airspace •Coastal location Wallops Range Instrumentation WFF Telemetry & Orbital Tracking Station FPQ-6 Radar •Telemetry •Radar •UHF transmitters •Real-time computer data display systems •Film/video tracking •Radio, intercom, and voice circuits •Weather measurement & forecasting Transmitter Site Camera Station Wallops Mobile Range Puerto Rico Campaign •Provides independent suborbital & orbital mission support at remote sites worldwide •Typical missions •Sounding rocket science campaigns •WFF ELV downrange support •Mobile ELV and X-vehicle missions •Recent Campaigns Kodiak Alaska, Australia, Brazil, Puerto Rico, Greenland, Kwajalein, Canary Islands Greenland Launcher Mobile Instrumentation Kodiak Star Launch Earth Science Research •Research activities include: •Atmospheric chemistry •Beach erosion •Arctic ice mapping •Hurricanes •Satellite Altimetry •Biological modeling •Coastal Zone Research Antarctic & Greenland Ice Mapping •Remote & in-situ instruments flown on aircraft, balloons, & rockets Coastal Zone Research •Worldwide data measurements •Cal/Val instrument support Laser & Radar Altimetry Wallops “Wave Tank” •Laboratories include: •Air-Sea Interaction Facility •Rain-Sea Interaction Facility Education Flight Projects • “Hands-on” opportunities for students of all ages to develop & fly experiments • NASA flight projects leveraged to create low-cost flight projects • Carriers include Rockets, Balloons, Aircraft & UAVs • “Piggy-back” often available • Students participate in • • • • • Experiment development Carrier integration Safety verification Mission operations Post-mission analysis • On-site student integration/lab facilities • Nationwide, real-time participation through Internet (e.g., web-casting) & the Student Ground Network Space Grant Consortium & Wallops • Virginia • 2 Members of VSGC Advisory Council • Sounding Rocket Programs • VGSC-Wallops MOU • Collaborative access to each other’s personnel and facilities • Cooperation between staff: extended visits at each other’s institutions • Maryland • MOU under negotiation SUBORBITAL AND SPECIAL ORBITAL PROJECTS DIRECTORATE Overview of the NASA Balloon Program Office (BPO) and Potential Student Opportunities Dr. Magdi Said Phone: (757) 824-1386 Fax: (757) 824-2149 [email protected] NASA Mid-Atlantic Regional Space Grant Meeting Charlottesville, Virginia September 13-15, 2006 NASA’s Scientific Balloons – Physical Dimensions & Size Comparison NASA Mid-Atlantic Regional Space Grant Meeting NASA’s Balloon Program The Balloon Program provides low cost, high altitude platforms to facilitate scientific exploration Largest balloon flown by NASA 59.6 MCF (1.7M m3) Highest altitude achieved by a NASA Balloon 160 k ft (4900 km) Normal float altitude 110-130k ft (33.5-39.6 km). Average number flown per year 20 balloons Average duration (ZP) 12-36 hours Longest Duration for ZP balloon (LDB) 42 days (Antarctica Dec/Jan 04) Payload capacity Up to 8000 Lbs. (3600 kg) NASA Mid-Atlantic Regional Space Grant Meeting Balloon Launch …. L a u n c h V i d e Balloon operations are o conducted under a NASA Contract by the Physical Science Laboratory of New Mexico State University located at the NASA Columbia Scientific Balloon Facility (CSBF) in Palestine, TX. NASA Mid-Atlantic Regional Space Grant Meeting Balloon Launch Sites Around the World With International Overflight Approval, Northern Hemisphere 21+ Day Flights Could Be Achieved BLAST Sweden To Canada Trajectory, June 12 to 16th, 2005 CREAM 41.9 Day 3-Circumpolar Trajectory Over Antarctica Dec 04 – Jan 05 NASA Mid-Atlantic Regional Space Grant Meeting Typical Science Payloads ….. CREAM - Cosmic Ray Energetics And Mass •Particle Astrophysics •NASA LDB Fight Duration Record Of Over 41 Days •Dec 16, 2004 – Jan 27, 2005 NASA Mid-Atlantic Regional Space Grant Meeting BESS – Balloon Experiment with Superconducting Spectrometer Particle Astrophysics Flown Over Antarctica Dec 13, 2004 – Dec 21, 2004 • • • Outreach Support and Student Opportunities The Balloon Program offers opportunities for students of all ages to access space Students learn to prepare space qualified payloads Students gain experience in space related technologies NASA Mid-Atlantic Regional Space Grant Meeting Specific Advantages for Students… Short project development cycle term (adequate for academic environment) Provide hands on experience during all phases of a mission. Payload almost always recoverable allowing for iterative learning Affordable NASA Mid-Atlantic Regional Space Grant Meeting Student Experiment Module on Balloon (SEM-B) What is it ? • • • Is an educational program that provides students opportunity to access space Open to students of all ages Based on a suitcase-like carrier with fixed dimensions SEM-B Suitcase NASA Mid-Atlantic Regional Space Grant Meeting Suitcase in flight configuration and ready for integration SEM-B Facts …. • • • • First suitcase flew in May 2004, last one in August 2006 (Total 13 cases) Thirty States participated in SEM-B opportunities Students from K-College participated in the SEM-B activities Students covered wide range of science disciplines NASA Mid-Atlantic Regional Space Grant Meeting Status of the SEM-B Activities as of September 06’ Alaska 1 Maine Vermont Washington Montana 2 Minnesota Idaho 1 Wyoming New York Wisconsin 1 Oregon 1 1 Illinois 2 2 Nevada Ohio Indiana Kansas Virginia 3 2 Kentucky Missouri 1 Hawaii Arizona New Mexico 1 States Utilized SEM-B (30) States have Not Utilized SEM-B (20+DC) 1 Elementary School (13) Oklahoma 1 1 High School (25) Regional (SchoolGrant District,Meeting Organization, Home School) (24) 1 Other Space Alabama 1 Mississippi Texas Louisiana 1 North Carolina South Carolina Arkansas 1 2 1 Middle School (25) (3) 1 College/University NASA Mid-Atlantic 1 2 Tennessee 1 Georgia 1 Massachusetts Rhode Island Connecticut 1 2 1 New Jersey Delaware Maryland 2 Colorado 1 1 2 West Virginia 3 3 Utah California 1 1 Pennsylvania 6 6 7 1 10 Iowa 2 2 4 1 3 1 3 2 2 Michigan South Dakota Nebraska 1 New Hampshire 1 North Dakota 3 Florida Washington DC High Altitude Student Platform (HASP) Is a collaboration between BPO and LSU providing student teams the opportunity to develop and operate an inexpensive platform that can be used to build and flight-test small payloads on a dedicated balloon platform. Support & flight test up to 12 student built payloads. Eight small payloads < 1 kg & four large payloads < 10 kg Fly to an altitude > 36 km for a duration of ~20 hours Cosmo-Cam Interactive video imaging system is used throughout the flight. NASA Mid-Atlantic Regional Space Grant Meeting HASP Experiments for FY06 First HASP payload contained 7 student payloads from 4 institutions as follows: University of Alabama – Huntsville: Infrared telescopes to remotely study the thermal characteristics of the balloon envelope (3 small) Texas A & M University: Video camera system to study remote sensing from high altitude (1 small) University of Louisiana – Lafayette: Nuclear emulsion stack to investigate high energy cosmic rays (1 large) Louisiana State University (Mechanical Eng.): Study the flow characteristics of various rocket nozzles as a function of altitude (1 large) Louisiana State University (Physics): Prototype of an accelerometer based inertial navigation system (1 small) NASA Mid-Atlantic Regional Space Grant Meeting HASP First Flight …. First flight was launched from Ft. Sumner, NM on September 4, 2006 aboard an 11.82 MCF balloon. Payload weight was 1000 LBS Float altitude was 122 KFT Total flight time was 18 HRS., 11 MIN. The flight was an operations and science success. It exceeded all preflight minimum requirements. The Call for Payload for FY07 has been released, available on HASP website. NASA Mid-Atlantic Regional Space Grant Meeting SEM-B & Other Student Opportunities Passive SEM-B*: self contained, no external interactions (e.g. seeds, personal products ..etc.) Semi-active SEM-B*: allows limited support by operations personnel prior to and/or after recovery (e.g. turning switches on/off, activating or deactivating certain devices … etc.) Active SEM-B*: will require compatibility checks with the science payload and may require power and communication support from the balloon instrumentation Non-SEM-B piggy back configuration – requires integration and coordination with the BPO, CSBF and PI (Scientist). Cost sharing missions: Example - HASP (LSU) * Requires coordination with and approval of the Scientist (PI) NASA Mid-Atlantic Regional Space Grant Meeting Testimonies …… Ballooning Contributions to NASA Strategic Objectives “The NASA Balloon Program was critical to my development as a scientist, both in graduate school and as a junior faculty member at Caltech. I can't imagine a better scientific training for experimental space science than the experience of building and launching a science payload on a balloon. You directly experience all the important steps: design to cost, schedule, weight, and power constraints; quality control and risk management; field operations; and reduction and analysis of data. The impact of the NASA Balloon Program goes far beyond the demonstration of technology and the direct science data that are produced - the scientists who ‘cut their teeth’ in the NASA Balloon Program are very often the leaders of today's NASA space science missions and programs.” Thomas A. Prince NASA Mid-Atlantic Regional Space Grant Meeting Caltech Prof. of Physics JPL Chief Scientist LISA Mission Scientist Ballooning Contributions to NASA Strategic Objectives “In my career as a scientist, astronaut, and as NASA's Chief Scientist, I often reflect back on the strength of the foundation upon which I was trained. As an undergraduate and as a graduate student I had the great fortune to perform experiments in high-energy astrophysics using high altitude balloons as a platform for access to space. The NASA scientific ballooning program provided me with the complete and quintessential scientific experience, going from concept to hardware, observations, and scientific analysis of the results. All in the time frame of a few years. The rich environment that NASA's sub-orbital program supports not only enables top quality science, but is also crucial as a training ground for the scientists who will be the principal investigators of tomorrow.” John M. Grunsfeld Astronaut (NASA ExChief Scientist) NASA Mid-Atlantic Regional Space Grant Meeting How to Contact NASA’s BPO ? Address: Wallops Flight Facility, Wallops Island, VA 23337 (Attention: Code 820) BPO Chief/Mr. David Pierce (757) 824-1453 BPO Assistant Chief/Mr. David Gregory (757) 824-2367 BPO Technologist/Outreach/ Dr. Magdi Said (757) 824-1386 BPO Secretary/Ms. Rebecca Gramlich (757) 824-1480 Office Fax Number (757) 824-2149 BPO Website: www.wff.nasa.gov/balloons For More info on HASP Contact: Professors T.G. Guzik and J.P. Wefel Dept. of Physics & Astronomy Louisiana State University Baton Rouge, LA U.S.A. (http://laspace.lsu.edu/hasp/) NASA Mid-Atlantic Regional Space Grant Meeting University Space Flight Opportunity Concept NASA Sounding Rocket Program Philip Eberspeaker September 14, 2006 Anatomy of a Sounding Rocket Scientific payload and NASA subsystems (4’ to 15’ long) Commercial rocket motors – some configurations may consist entirely of surplus rocket motors. Surplus rocket motors – NASA builds hardware to adapt systems for civilian use. Sounding Rocket Vehicles Wallops Flight Facility provides a stable of 13 vehicles. This variety allows the program to tailor the vehicle performance to the scientific requirements. Key Considerations • Cost to NASA must be minimized • NASA work effort needs to be kept to a minimum • Cost of launch operations must be minimized • The Sounding Rocket Program needs to realize some benefit from the investment Potential Approach • Surplus launch vehicle – Terrier-Orion most likely candidate • Standardized payload configuration – – – – – Reusable Set power, telemetry, and timing support Set experiment volume 4 experiments per flight Base-line payload exists (SubSEM) • Launch from Wallops Flight Facility • Proposed flight experiments should support sounding rocket program technology needs Sub-orbital Student Experiment Module (SubSEM) Vehicle Stack Water recovery operations Terrier-Orion on the Launch Pad Lift-off SubSEM payload after recovery Experiment Configuration Experiment Bay - Four Experiments Sample Experiment Proposed Experiment Support Services • 16 Analog Telemetry Data Channels – – – – Standard interface connector 0-5 VDC signals (current configuration) Data Rate: Up to 20,000 words per second Digital channels could be considered • 4 Timer Functions – Standard interface connector – Capable on/off cycling • 12VDC (or 28VDC) Power Supply – Current limited to protect other experiments Potential Experiment Topics • Component test flights – Battery technologies – New GPS receivers – Sensors • Development of new techniques – Deployment mechanisms – Attitude determination – Ethernet communications (internal) • Vibration, acoustics and flight loads research Alternate Approach • Small piggy-back module on science missions • No control over location and schedule • Weight must be minimized • Fully autonomous system is required – – – – Power Data recording (no RF down link) Turn on at lift-off No pre-launch experiment control Contacts Suggestions and implementation concerns can be communicated to: Philip Eberspeaker 757-824-2202 [email protected]