SMALL SATELLITE CONFERENCE Thomas H
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Solar Sail Propulsion for Deep Space Exploration
Solar Sail Propulsion for Deep Space Exploration Les Johnson NASA George C. Marshall Space Flight Center NASA Image We tend to think of space as being big and empty… NASA Image Space Is NOT Empty. We can use the environments of space to our advantage NASA Image Solar Sails Derive Propulsion By Reflecting Photons Solar sails use photon “pressure” or force on thin, lightweight, reflective sheets to produce thrust. 4 NASA Image Real Solar Sails Are Not “Ideal” Billowed Quadrant Diffuse Reflection 4 Thrust Vector Components 4 Solar Sail Trajectory Control Solar Radiation Pressure allows inward or outward Spiral Original orbit Sail Force Force Sail Shrinking orbit Expanding orbit Solar Sails Experience VERY Small Forces NASA Image 8 Solar Sail Missions Flown Image courtesy of Univ. Surrey NASA Image Image courtesy of JAXA Image courtesy of The Planetary Society NanoSail-D (2010) IKAROS (2010) LightSail-1 & 2 CanX-7 (2016) InflateSail (2017) NASA JAXA (2015/2019) Canada EU/Univ. of Surrey The Planetary Society Earth Orbit Interplanetary Earth Orbit Earth Orbit Deployment Only Full Flight Earth Orbit Deployment Only Deployment Only Deployment / Flight 3U CubeSat 315 kg Smallsat 3U CubeSat 3U CubeSat 10 m2 196 m2 3U CubeSat <10 m2 10 m2 32 m2 9 Planned Solar Sail Missions NASA Image NASA Image NASA Image Near Earth Asteroid Scout Advanced Composite Solar Solar Cruiser (2025) NASA (2021) NASA Sail System (TBD) NASA Interplanetary Interplanetary Earth Orbit Full Flight Full Flight Full Flight 100 kg spacecraft 6U CubeSat 12U CubeSat 1653 m2 86 -
KPLO, ISECG, Et Al…
NationalNational Aeronautics Aeronautics and Space and Administration Space Administration KPLO, ISECG, et al… Ben Bussey Chief Exploration Scientist Human Exploration & Operations Mission Directorate, NASA HQ 1 Strategic Knowledge Gaps • SKGs define information that is useful/mandatory for designing human spaceflight architecture • Perception is that SKGs HAVE to be closed before we can go to a destination, i.e. they represent Requirements • In reality, there is very little information that is a MUST HAVE before we go somewhere with humans. What SKGs do is buy down risk, allowing you to design simpler/cheaper systems. • There are three flavors of SKGs 1. Have to have – Requirements 2. Buys down risk – LM foot pads 3. Mission enhancing – Resources • Four sets of SKGs – Moon, Phobos & Deimos, Mars, NEOs www.nasa.gov/exploration/library/skg.html 2 EM-1 Secondary Payloads 13 CUBESATS SELECTED TO FLY ON INTERIM EM-1 CRYOGENIC PROPULSION • Lunar Flashlight STAGE • Near Earth Asteroid Scout • Bio Sentinel • LunaH-MAP • CuSPP • Lunar IceCube • LunIR • EQUULEUS (JAXA) • OMOTENASHI (JAXA) • ArgoMoon (ESA) • STMD Centennial Challenge Winners 3 3 3 Lunar Flashlight Overview Looking for surface ice deposits and identifying favorable locations for in-situ utilization in lunar south pole cold traps Measurement Approach: • Lasers in 4 different near-IR bands illuminate the lunar surface with a 3° beam (1 km spot). Orbit: • Light reflected off the lunar • Elliptical: 20-9,000 km surface enters the spectrometer to • Orbit Period: 12 hrs distinguish water -
Explore Digital.Pdf
EXPLORE “sic itur ad astra” ~ thus you shall go to the stars EXPERTISE FOR THE MISSION We’ve built more interplanetary spacecraft than all other U.S. companies combined. We’re ready for humanity’s next step, for Earth, the Sun, our planets … and beyond. We do this for the New capability explorers. And for us for a new space era Achieving in space takes tenacity. Lockheed Martin brings more We’ve never missed a tight (and finite) capability to the table than ever planetary mission launch window. before, creating better data, new Yet, despite how far we go, the most images and groundbreaking ways to important technologies we develop work. And we’re doing it with smarter improve life now, closer to home. factories and common products, Here on Earth. making our systems increasingly affordable and faster to produce. HALF A CENTURY AT MARS Getting to space is hard. Each step past that is increasingly harder. We’ve been a part of every NASA mission to Mars, and we know what it takes to arrive on another planet and explore. Our proven work includes aeroshells, autonomous deep space operations or building orbiters and landers, like InSight. AEROSHELLS VIKING 1 VIKING 2 PATHFINDER MARS POLAR SPIRIT OPPORTUNITY PHOENIX CURIOSITY INSIGHT MARS 2020 1976 1976 1996 LANDER 2004 2018 2008 2012 2018 2020 1999 ORBITERS MARS OBSERVER MARS GLOBAL MARS CLIMATE MARS ODYSSEY MARS RECONNAISSANCE MAVEN 1993 SURVEYOR ORBITER 2001 ORBITER 2014 1997 1999 2006 LANDERS VIKING 1 VIKING 2 MARS POLAR PHOENIX INSIGHT 1976 1976 LANDER 2008 2018 1999 Taking humans back to the Moon – We bring solutions for our customers that include looking outside our organization to deliver the best science through our spacecraft and operations expertise. -
Advanced Exploration Systems
National Aeronautics and Space Administration National Aeronautics and Space Administration Advanced Exploration Systems 10 October 2017 JASON CRUSAN Director, Advanced Exploration Systems NASA Headquarters 1 2 PHASE 1 Deep Space Gateway (DSG) Concept Phase 2: Deep Space Transport Orion PHASE 2 Deep Space Gateway HABITATION CAPABILITY Systems to enable crews to live and work safely in deep space. Capabilities and systems will be used in conjunction with Orion and SLS on exploration missions in cislunar space and beyond. 5 DEEP SPACE HABITATION SYSTEMS TODAY FUTURE Habitation Systems Elements Space Station Deep Space LIFE SUPPORT Excursions from Earth are possible with artificially produced breathing air, drinking water and other conditions for survival. 42% O Recovery from CO 2 2 75%+ O2 Recovery from CO2 90% H O Recovery 2 98%+ H2O Recovery Atmosphere Waste Management Management < 6 mo mean time before failure >30 mo mean time before Water (for some components) failure Management ENVIRONMENTAL MONITORING NASA living spaces are designed with controls and integrity that ensure the comfort and safety of inhabitants. Limited, crew-intensive On-board analysis capability on-board capability with no sample return Identify and quantify species Pressure Particles Chemicals Reliance on sample return to and organisms in air & water O & N Earth for analysis 2 2 Moisture Microbes Sound CREW HEALTH Astronauts are provided tools to perform successfully while preserving their well-being and long-term health. Bulky fitness equipment Smaller, efficient equipment Limited medical capability Onboard medical capability Monitoring Diagnostics Food Storage & Management Frequent food system resupply Long-duration food system Exercise Treatment EVA: EXTRA- Long-term exploration depends on the ability to physically investigate the unknown for VEHICULAR ACTIVITY resources and knowledge. -
Space Launch System Program March 1, 2018
https://ntrs.nasa.gov/search.jsp?R=20180003498 2019-08-31T15:55:45+00:00Z National Aeronautics and Space Administration 5 . 4 . 3 .SPACE . 2 . 1 . LAUNCH SYSTEM CubeSats - To The Moon & Beyond Scott Spearing CubeSat Subject Matter Expert Space Launch System Program March 1, 2018 www.nasa.gov/sls www.nasa.gov/sls SLS BLOCK 1 EXPLORATION MISSION-1 (EM-1) Forward Ring Launch Abort System Secondary Payloads Electrical Panels Cabling Orion Avionics Box (2 places) Interim Cryogenic Propulsion Stage Launch Vehicle Stage Adapter OSA Diaphragm Core Stage Secondary Payload Brackets (13) Boosters Isogrid Barrel Panels Access Cover Aft Ring (2 places) Orion Stage Adapter (OSA) www.nasa.gov/sls 0418 EM-1 OSA SECONDARY PAYLOAD ACCOMMODATIONS Secondary Payload Avionics Box Cabling 6U CubeSat Payload 6U CubeSat Secondary Payload Dispenser Brackets (13) (PSC) Secondary Payload Mounting Bracket LEGEND: SLS Provided PD Provided www.nasa.gov/sls 0418 EM-1 SYSTEM DESCRIPTION AND PURPOSE Expand and fully utilize the SLS capabilities for exploration purposes without causing harm or inconvenience to SLS or its primary payload. • Thirteen (max capability 17) 6U payload locations • 6U volume/mass is the current standard OSA (14 kg payload mass) Diaphragm • Payloads will be “powered off” from turnover through Orion separation and ~Ø156” (13’) payload deployment • Payload Deployment System Avionics Unit; payload deployment will begin with pre-loaded OSA ~21° sequence following Orion separation and ~22° ICPS disposal burn • Payload requirements captured in Interface -
Changing Human Spaceflight Exploration Plans
National Aeronautics and Space Administration NASA’s Changing Human Spaceflight Exploration Plans FISO – 6-13-2018 John Guidi Deputy Director, Advanced Exploration Systems Division Human Exploration and Operations Mission Directorate NASA The US Space Policy Directive-1 “Lead an innovative and sustainable program of exploration with commercial and international partners to enable human expansion across the solar system and to bring back to Earth new knowledge and opportunities. Beginning with missions beyond low-Earth orbit, the United States will lead the return of humans to the Moon for long-term exploration and utilization, followed by human missions to Mars and other destinations.” 2 2016 3 3 National Aeronautics and EXPANDING HUMAN PRESENCE IN PARTNERSHIP ~2017Space Administration CREATING ECONOMIC OPPORTUNITIES, ADVANCING TECHNOLOGIES, AND ENABLING DISCOVERY 2020s After 2030 Leaving the Earth-Moon Operating in the Lunar System and Reaching Mars Now Vicinity (proving ground) Orbit Using the International Space Station Phase 0 Phase 1 Phase 2 Continue research and Begin missions in cislunar Complete next deep testing on ISS to solve space. Initiate next key space capability and exploration challenges. deep space capability. checkout. Evaluate potential for lunar resources. Develop standards. 4 EXPLORATION CAMPAIGN 2018 5 Funding: FY2019 Presidential Budget Request Highlights • Provides $19.9B, including $10.5B to lead an innovative • Develops a series of progressively more capable and sustainable campaign of exploration and lead the robotic lunar missions to the surface of the moon using return of humans to the Moon for long-term exploration innovative acquisition approaches while meeting and utilization followed by human missions to Mars and national exploration and scientific objectives. -
Smallsats Supporting Deep Space Human Exploration
National Aeronautics and Space Administration SmallSats supporting Deep Space Human Exploration August 06, 2018 Andres Martinez, Program Executive, Advanced Exploration Systems, HEOMD, NASA HQ Background about me… 2 National Advisory Committee for Aeronautics 3 National Aeronautics and Space Administration 4 NASA 5 Small Spacecraft Technology Program 6 NASA’S DEEP SPACE EXPLORATION SYSTEM The Orion spacecraft and Space Launch System rocket, launching from a modernized Kennedy spaceport is foundational to extending human presence deeper into the solar system. 7 EM-1 Secondary Payloads 13 CUBESATS SELECTED TO FLY ON EM-1 INTERIM • Lunar Flashlight CRYOGENIC • Near Earth Asteroid Scout PROPULSION STAGE • Bio Sentinel • LunaH-MAP • CuSP • Lunar IceCube • LunIR • EQUULEUS (JAXA) • OMOTENASHI (JAXA) • ArgoMoon (ESA) • STMD Centennial Challenge Winners: CU-E3, CisLunar Explorers, & Team Miles HEOMD/AES Deep Space SmallSats: SLS EM-1 Secondary Payloads Lunar IceCube Lunar Flashlight NEA Scout LunIR AES SmallSat Missions selected to contribute to key Human Exploration Strategic Knowledge Gaps and to Advance Key Technologies BioSentinel 10 HEOMD/AES Deep Space SmallSats: Deep Space Station 17 (DSS-17) LRO Demonstrations: • Routinely Tracking LRO at S-band • Intermediate Frequency (IF) Systems and DSN Downlink Equipment (DCD, MarCO Demonstrations: DTT) Verified • Downlink Using X-Band Feed and DSN Equipment • LRO Telemetry Blocks Sent Directly • Downlink Using X-Band Feed and MarCO Receiver System Expands DSN capabilities by utilizing from DSS-17 to JPL DSOC over the • OMSPA Using X-Band Feed and Custom SDR-based NASA Mission Backbone- verifying Multiple Receiver System non-NASA assets to provide DSS-17 Signal Path communication and navigation services FirstFirst OMSPA OMSPA Demonstration Demonstration to small spacecraft missions to the withwith a a CubeSat CubeSat Moon and inner solar system. -
Nasa's Space Launch System: Deep
https://ntrs.nasa.gov/search.jsp?R=20180005407 2020-02-21T02:27:56+00:00Z NASA’S SPACE LAUNCH SYSTEM: DEEP-SPACE OPPORTUNITIES FOR SMALLSATS 4S Symposium Kimberly Robinson, Ph.D. Payloads Manager Carole McLemore, Ph.D. Secondary Payloads Integration Manager Space Launch System Program May 29, 2018 0496 0496 NASA’S EXPLORATION PLANS 0496 SLS – ENABLING HUMAN EXPLORATION EXPLORATION CLASS: DEEP SPACE CAPABILITIES • Five times more volume than any contemporary heavy lift vehicle VOLUME Orion 8m fairing • Only vehicle that can carry the Orion and a co- with with large manifested payload to the Moon Science aperture Missions telescope • Block 1: Can launch 60% more mass than any contemporary launch vehicle MASS • Block 2: Mars-enabling capability of greater than Contemporary SLS Block 1 SLS Block 2 Heavy Lift Exploration Exploration 45 metric tons to Trans Lunar Injection Class Class • Reduce transit times by half or greater to the outer DEPARTURE solar system ENERGY 0496 SLS BLOCK 1 CONFIGURATION FOR EM-1 Launch Abort System (LAS) Crew Module (CM) Service Module (SM) Encapsulated Service Module (ESM) Panels Spacecraft Adapter Orion Stage Adapter Orion Spacecraft Lockheed Martin 5 Segment Solid Rocket Boosters (2) Orbital ATK Interim Cryogenic Propulsion Stage (ICPS) Boeing/United Launch Alliance Launch Vehicle Stage Adapter Teledyne Brown Engineering Core Stage & Avionics Boeing RS-25 Engines (4) Aerojet Rocketdyne 0496 SOLID ROCKET BOOSTERS 0496 ENGINES 0496 CORE STAGE 0496 IN-SPACE STAGE AND ADAPTERS 0496 EXPLORATION MISSION-1 FULL SYSTEMS -
Nasa's Space Launch System: Deep-Space Opportunities
https://ntrs.nasa.gov/search.jsp?R=20180005407 2019-08-31T14:51:15+00:00Z NASA’S SPACE LAUNCH SYSTEM: DEEP-SPACE OPPORTUNITIES FOR SMALLSATS 4S Symposium Kimberly Robinson, Ph.D. Payloads Manager Carole McLemore, Ph.D. Secondary Payloads Integration Manager Space Launch System Program May 29, 2018 0496 0496 NASA’S EXPLORATION PLANS 0496 SLS – ENABLING HUMAN EXPLORATION EXPLORATION CLASS: DEEP SPACE CAPABILITIES • Five times more volume than any contemporary heavy lift vehicle VOLUME Orion 8m fairing • Only vehicle that can carry the Orion and a co- with with large manifested payload to the Moon Science aperture Missions telescope • Block 1: Can launch 60% more mass than any contemporary launch vehicle MASS • Block 2: Mars-enabling capability of greater than Contemporary SLS Block 1 SLS Block 2 Heavy Lift Exploration Exploration 45 metric tons to Trans Lunar Injection Class Class • Reduce transit times by half or greater to the outer DEPARTURE solar system ENERGY 0496 SLS BLOCK 1 CONFIGURATION FOR EM-1 Launch Abort System (LAS) Crew Module (CM) Service Module (SM) Encapsulated Service Module (ESM) Panels Spacecraft Adapter Orion Stage Adapter Orion Spacecraft Lockheed Martin 5 Segment Solid Rocket Boosters (2) Orbital ATK Interim Cryogenic Propulsion Stage (ICPS) Boeing/United Launch Alliance Launch Vehicle Stage Adapter Teledyne Brown Engineering Core Stage & Avionics Boeing RS-25 Engines (4) Aerojet Rocketdyne 0496 SOLID ROCKET BOOSTERS 0496 ENGINES 0496 CORE STAGE 0496 IN-SPACE STAGE AND ADAPTERS 0496 EXPLORATION MISSION-1 FULL SYSTEMS -
Enabling a New Generation of Lunar Exploration Stephen D
NASA’s Space Launch System: Enabling a New Generation of Lunar Exploration Stephen D. Creech NASA’s Space Launch System Program Spacecraft/Payload Integration & Evolution (SPIE) Office Mailstop XP50, Marshall Space Flight Center, AL 35812 256-544-9365 [email protected] Abstract—Following two decades of operational experience in 1. NASA’S LUNAR EXPLORATION low-Earth orbit (LEO), NASA has turned its focus once again to deep space exploration. The Agency is building the Space CAMPAIGN Launch System (SLS) to take astronauts and cargo to the Moon With the signing of Space Policy Directive 1, the U. S. and send robotic spacecraft deep into the solar system. Offering Administration has directed NASA to focus resources on unmatched performance, departure energy and payload deep space exploration. Specifically, the policy directs the capacity, SLS is designed to evolve into progressively more powerful configurations, enabling a new generation of human Agency to: exploration of the Moon in preparation for future missions to Mars. The first build of the Block 1 vehicle is nearly complete Lead an innovative and sustainable program of for Exploration Mission-1 (EM-1), the first integrated flight of exploration with commercial and international SLS and the Orion crew vehicle. EM-1 will send an uncrewed partners to enable human expansion across the Orion to a distant retrograde lunar orbit in order to test and solar system and to bring back to Earth new verify new systems, and along the way will deploy 13 6U-class knowledge and opportunities. Beginning with CubeSats in deep space along the upper stage disposal missions beyond low-Earth orbit, the United States trajectory after separation from Orion. -
Cubesat-Sized Space Microcryocooler
CubeSat-Sized Space Microcryocooler 33rd Annual AIAA/USU Conference on Small Satellites Dr. Jeffrey Olson Principal Research Scientist Lockheed Martin Space Advanced Technology Center, Palo Alto California Motivation Cryogenic instruments on small satellites and deep space missions require compact, low-mass cryocoolers The trend toward Many missions require operational lifetime of several years or more smaller satellites is creating a need Some missions have very challenging for smaller environmental conditions space-quality cryocoolers Jeff Olson © 2019 Lockheed Martin Corporation, all rights reserved. Approved for Public Disclosure 2 Description of Stirling Cryocooler Hot Piston Regenerator Porous matrix (passive thermal storage) Cold Piston Hot End Translation Cold End Translation Compression Expansion Time Jeff Olson © 2019 Lockheed Martin Corporation, all rights reserved. Approved for Public Disclosure 3 Space Cryocooler Configuration Hot Piston: Power input Compressor Hot Heat Exchanger: Heat rejection Pulse Tube Cold Head Regenerator Cold Heat Exchanger: Cooling Power Cold Piston: Work extraction Work Flow Moving cold part is Replace moving cold one of the primary part with passive causes of failure in a components Stirling cryocooler Jeff Olson © 2019 Lockheed Martin Corporation, all rights reserved. Approved for Public Disclosure 4 Long Life Compressor Features Clearance seals Linear Flexure Bearings (minimal (designed to be within Lockheed Martin compressors have rubbing) infinite fatigue limit) external motor coils (no electrical penetrations into pressure vessel Opposed motion for minimal There has never been vibration an on-orbit failure of a Oscillating pressure to pulse tube cryocooler with cryocooler cold head an Oxford-style compressor in over 200 years of Long-life space configuration developed in 1990s at Oxford University operational time Jeff Olson © 2019 Lockheed Martin Corporation, all rights reserved. -
Navigating Smallsat Development: Where to Begin and What to Expect
Navigating SmallSat Development: Where to Begin and What to Expect Dr. Charles D. Norton Special Advisor, Small Spacecraft Missions, NASA SMD Associate Chief Technologist, NASA Jet Propulsion Laboratory / CalTech August 2020 Clearance: NF-1676 20205006873 Aug. 4, 1971 Apollo-15 Particles and Fields Apollo Subsatellites Subsatellite Met objectives to study the plasma, particle, and magnetic field environment of the Moon and to map the lunar gravity field Mass of 35.6 kg carrying 3 instruments: magnetometer, S- band transponder, and charged particle detector Courtesy: NASA Space Science Data Center Catalog David Scott, Alfred Worden, and James Irwin 2 NASA Annual Expenditures for Science Missions In FY15 Millions of Dollars for 57 Years (1969 – 2026) National Academies of Sciences, Engineering, and Medicine. 2017. Powering Science—NASA’s Large Strategic Science Missions. Washington, DC: The National Academies Press. https://doi.org/10.17226/24857 Aqua Aura Juno MO MER ICESat 2 SIM Spitze r 3 Topics for Discussion The Basics Mission Formulation Realities of Flight Development Access to Space Mission Operations Closing Remarks 4 Fundamentals of Small Spacecraft Spectrum of Satellite Development ISS The Basics The Rideshare Picosatellite CubeSat/Nanosatellite PocketSat (0.1 – 1 kg) MCubed (1 – 10 kg) ESPA-Ring Payload Port Limit (450 kg) New SMD Working Definition A spacecraft that is interface Dedicated compatible with an ESPA Ring, a dedicated small or medium-lift launch vehicle, or a containerized dispenser, and with an upper mass Microsatellite