CAL POLY CORPORATION

SUPPORT POLY PICOSATELLITE ORBITAL DEPLOYERS (PPOD0 FIVE YEAR IDIQ CONTRACT.

IGF::CT::IGF - WATER CONSERVATION TECHNICAL SUPPORT

STATEMENT OF WORK FOR DEVELOPMENT OF THE INTEGRATED MODELING AND VERIFICATION OF HYBRID WING-BODY, LOW NOISE ESTOL AIRCRAFT RESEARCH OPPORTUNITIES IN AERONAUTICS - 2006 (ROA-2006), NRA-NNH06ZEA001N-SSFW2, PROPOSAL: 06-SSFW2-06-0058 1.0 INTRODUCTION/BACKGROUND THIS EFFORT IS DIVIDED INTO TWO PHASES. PHASE I IS A 1-YEAR BASE PERIOD, AND PHASE II IS A 2-YEAR OPTION PERIOD. THE PURPOSE OF THIS EFFORT IS TO DEVELOP AND VALIDATE PREDICTIVE CAPABILITIES FOR THE DESIGN AND PERFORMANCE OF CRUISE EFFICIENT, SHORT TAKE-OFF AND LANDING (CESTOL) SUBSONIC AIRCRAFT, AND TO VALIDATE PREDICTIVE CAPABILITIES FOR AN ESTIMATE OF CESTOL AIRCRAFT NOISE DURING TAKEOFF AND LANDING. FOR PHASE I (I.E., YEAR 1 BASE PERIOD), THESE METHODOLOGIES WILL BE THEN BE USED TO ACHIEVE THE FINAL OBJECTIVE OF YEAR 1, WHICH IS TO SELECT AND FURTHER REFINE ONE CESTOL CONCEPT AND THEN TO COMPLETE A PRELIMINARY DESIGN OF A LARGE SCALE WIND TUNNEL MODEL AND TEST. FOR PHASE II (I.E., YEARS 2 AND 3 OPTION PERIOD), THE WIND TUNNEL DESIGN AND CONSTRUCTION IS TO BE COMPLETED IN YEAR 2, AND A LARGE SCALE WIND TUNNEL TEST IS TO BE COMPLETED IN YEAR 3. THE FINAL OBJECTIVE OF PHASE II IS THE DEVELOPMENT VERIFICATION OF PREDICTIVE CODES FOR THESE ADVANCED POWERED-LIFT CONCEPTS AND THE GENERATION OF AN OPEN COLLECTION OF WIND TUNNEL DATA THAT CAN BE USED BY MODELERS TO IMPROVE THE CAPABILITY OF MODELING THESE COMPLEX FLOWS. IT IS INTENDED THAT THE PHASE I AND PHASE II (IF OPTION IS EXERCISED) EFFORT WILL ADDRESS THE FOLLOWING TOPICS:  LOW-SPEED AERODYNAMIC CHARACTERISTICS UP TO AND BEYOND MAXIMUM LIFT VIA A COMBINATION OF COMPUTATIONAL AND EXPERIMENTAL EFFORTS IN ORDER TO OBTAIN A MORE COMPLETE PICTURE OF THE FLOW PHYSICS.  ACOUSTIC CHARACTERISTICS OF A LOW-NOISE HYBRID WING-BODY SYSTEM VIA EXPERIMENTAL EFFORTS AND NOISE SIGNATURE MODELING TO ANALYZE NOT JUST THE NOISE GENERATED BY THE VEHICLE, BUT ALSO TO ANALYZE THE NOISE FOOTPRINT AROUND THE AIRPORT DURING TAKEOFF AND LANDING. 2.0 SCOPE OF WORK PHASE I WILL CONDUCT A PRELIMINARY DESIGN STUDY TO DETERMINE THE HYBRID WING-BODY DESIGN TO BE ANALYZED IN PHASE II, INCLUDING POWERED LIFT AERODYNAMIC STUDIES, BOTH COMPUTATIONAL AND EXPERIMENTAL, TO BETTER UNDERSTAND OF THE FLOW PHYSICS ASSOCIATED WITH USING THE PROPULSION SYSTEM TO IMPROVE THE AIRCRAFT LIFTING CAPABILITY. PHASE II WILL EXPAND THE UNDERSTANDING OF THE PHYSICS OF THE FLOW FIELD ASSOCIATED WITH POWERED LIFT CONFIGURATIONS. THE DESIGN DETERMINED FROM PHASE I WILL BE THE FOCUS OF BOTH THE EXPERIMENTAL AND COMPUTATIONAL EFFORTS. THE PROPULSION MODELING WILL BE FOCUSED ON METHODS OF IMPROVING THE AERODYNAMIC PREDICTIVE CAPABILITIES. THE LARGE SCALE WIND TUNNEL MODEL EFFORT IN YEAR 2 WILL FOCUS ON FINALIZING THE WIND TUNNEL MODEL, ASSEMBLING THE TEST PLAN, AND SCHEDULING THE EXPERIMENT IN THE CHOSEN FACILITY. YEAR 3 FOR THE LARGE SCALE WIND TUNNEL MODEL EFFORT WILL FOCUS ON PERFORMING THE EXPERIMENTS, ANALYZING THE RESULTS, AND PREPARING THE RESULTS FOR RELEASE. PHASE II WILL CONCLUDE WITH THE RELEASE OF THE ENTIRE DATA (INCLUDING WIND TUNNEL GEOMETRIES, RESULTING DATA, COMPUTATIONAL GEOMETRY MODELS AND CFD CONFIGURATION FILES) TO NASA AND THE GENERAL RESEARCH COMMUNITY, IF POSSIBLE. THE CONTRACTOR SHALL NOT CONSIDER ANY DATA GENERATED FROM THIS EFFORT AS PROPRIETARY AND WILL RELEASE ALL OF THE DATA THAT IT IS LEGALLY ALLOWED TO RELEASE TO THE GENERAL RESEARCH COMMUNITY. NASA WILL ENSURE THAT AS MUCH OF THESE RESULTS AS POSSIBLE ARE ABLE TO BE RELEASED TO THE GENERAL RESEARCH COMMUNITY WITHOUT LEGAL RESTRICTION.

SMALL SATELLITE PPODS

POLY PICOSATELLITE ORBITAL DEPLOYER (P-POD)

MISSION SUPPORT FOR POLY PICOSATELLITE ORBITAL DEPLOYERS.

SOIL TESTING

P-POD CONTAINER

FY21 CS CAL POLY. FIVE DAY DIGITAL FORENSICS CLASS FOR FY2021 CYBERSHIELD EVENT.

DIGITAL FORENSICS COURSE

''IGF::OT::IGF'' ASSISTANT BIOLOGIST TO DEVELOP QUANTITATIVE METRICES OF GRAXIN INTENSITY

PURCHASE OF FLIGHT READY P-POD

FIELD-BASED STUDIES OF GIANT KANGAROO RATS AND SPINY LIZARDS

BASE TEST-POD TASK

RECONFIGURABLE NANOSAT TECHNOLOGY TES

STRATEGY CONTRACT

STRATEGY CONTRACT

TEST POD AND ON SITE TRAINING AND TEST SUPPORT

P-POD REFURBISHMENT AND FLIGHT CERTIFICATION TESTING

3U TESTPOD

BULL ; LIVESTOCK ANIMAL FOR FARM OPN

CATCH CANS/STANDS TO BE USED AS A COMPENENT OF THE IRRIGATION AUDIT KITS.

BULL FOR FCC LOMPOC FARM OPERATION

VIDEO TAPING SERVICES FOR DIABLO CANYON PUBLIC MEETING

UPDATE TO THE CUBESAT 101: BASIC CONCEPTS AND PROCESSES FOR FIRST-TIME CUBESAT DOCUMENT

DEVELOP. OF MODERNIZATION RECOM

CUBESAIL MISSION LAUNCH SEGMENT SUPPORT

ASTROBIONICS PROGRAM SYSTEMS ENGINEERING AND DESIGN SUPPORT FOR SAMLL SATELLITE DIVISION

THE CCC WILL FUND A COLLEGE STUDENT TO SERVE AS A LIASON BETWEEN USDA FOREST SERVICE AND CAL POLY SAN LUIS OBISPO. AMEND #1 - CHANGE JOB CODE FROM IDP221 TO NFTM21. PERIOD OF PERFORMANCE FROM 10-01-2005 TO 09-30-2006.