NASA's Space Launch System
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Human Mars Architecture
National Aeronautics and Space Administration Human Mars Architecture Tara Polsgrove NASA Human Mars Study Team 15th International Planetary Probe Workshop June 11, 2018 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 EXPLORATION CAMPAIGN Gateway Initial ConfigurationLunar Orbital Platform-Gateway (Notional) Orion 4 5 A Brief History of Human Exploration Beyond LEO America at DPT / NEXT NASA Case the Threshold Constellation National Studies Program Lunar Review of Commission First Lunar Architecture U.S. Human on Space Outpost Team Spaceflight Plans Committee Pathways to Exploration Columbia Challenger 1980 1990 2000 2010 Bush 41 Bush 43 7kObama HAT/EMC MSC Speech Speech Speech Report of the 90-Day Study on Human Exploration of the Moon and Mars NASA’s Journey to National Aeronautics and November 1989 Global Leadership Space Administration Mars Exploration and 90-Day Study Mars Design Mars Design Roadmap America’s Reference Mars Design Reference Future in Reference Mission 1.0 Exploration Architecture Space Mission 3.0 System 5.0 Exploration Architecture Blueprint Study 6 Exploring the Mars Mission Design Tradespace • A myriad of choices define -
Mission to Jupiter
This book attempts to convey the creativity, Project A History of the Galileo Jupiter: To Mission The Galileo mission to Jupiter explored leadership, and vision that were necessary for the an exciting new frontier, had a major impact mission’s success. It is a book about dedicated people on planetary science, and provided invaluable and their scientific and engineering achievements. lessons for the design of spacecraft. This The Galileo mission faced many significant problems. mission amassed so many scientific firsts and Some of the most brilliant accomplishments and key discoveries that it can truly be called one of “work-arounds” of the Galileo staff occurred the most impressive feats of exploration of the precisely when these challenges arose. Throughout 20th century. In the words of John Casani, the the mission, engineers and scientists found ways to original project manager of the mission, “Galileo keep the spacecraft operational from a distance of was a way of demonstrating . just what U.S. nearly half a billion miles, enabling one of the most technology was capable of doing.” An engineer impressive voyages of scientific discovery. on the Galileo team expressed more personal * * * * * sentiments when she said, “I had never been a Michael Meltzer is an environmental part of something with such great scope . To scientist who has been writing about science know that the whole world was watching and and technology for nearly 30 years. His books hoping with us that this would work. We were and articles have investigated topics that include doing something for all mankind.” designing solar houses, preventing pollution in When Galileo lifted off from Kennedy electroplating shops, catching salmon with sonar and Space Center on 18 October 1989, it began an radar, and developing a sensor for examining Space interplanetary voyage that took it to Venus, to Michael Meltzer Michael Shuttle engines. -
Preparation of Papers for AIAA Journals
ASCEND 10.2514/6.2020-4000 November 16-18, 2020, Virtual Event ASCEND 2020 Cryogenic Fluid Management Technologies Enabling for the Artemis Program and Beyond Hans C. Hansen* and Wesley L. Johnson† NASA Glenn Research Center, Cleveland, Ohio, 44135, USA Michael L. Meyer‡ NASA Engineering Safety Center, Cleveland, Ohio, 44135, USA Arthur H. Werkheiser§ and Jonathan R. Stephens¶ NASA Marshall Space Flight Center, Huntsville, Alabama, 35808, USA NASA is endeavoring on an ambitious return to the Moon and eventually on to Mars through the Artemis Program leveraging innovative technologies to establish sustainable exploration architectures collaborating with US commercial and international partners [1]. Future NASA architectures have baselined cryogenic propulsion systems to support lunar missions and ultimately future missions to Mars. NASA has been investing in maturing CFM active and passive storage, transfer, and gauging technologies over the last decade plus primarily focused on ground development with a few small- scale microgravity fluid experiments. Recently, NASA created a Cryogenic Fluid Management (CFM) Technology Roadmap identifying the critical gaps requiring further development to reach a technology readiness level (TRL) of 6 prior to infusion to flight applications. To address the technology gaps the Space Technology Mission Directorate (STMD) strategically plans to invest in a diversified CFM portfolio approach through ground and flight demonstrations, collaborating with international partners, and leveraging Public Private Partnerships (PPPs) opportunities with US industry through Downloaded by Michele Dominiak on December 23, 2020 | http://arc.aiaa.org DOI: 10.2514/6.2020-4000 the Tipping Point and Announcement of Collaborative Opportunities (ACO) solicitations. Once proven, these system capabilities will enable the high performing cryogenic propellant systems needed for the Artemis Program and beyond. -
JUICE Red Book
ESA/SRE(2014)1 September 2014 JUICE JUpiter ICy moons Explorer Exploring the emergence of habitable worlds around gas giants Definition Study Report European Space Agency 1 This page left intentionally blank 2 Mission Description Jupiter Icy Moons Explorer Key science goals The emergence of habitable worlds around gas giants Characterise Ganymede, Europa and Callisto as planetary objects and potential habitats Explore the Jupiter system as an archetype for gas giants Payload Ten instruments Laser Altimeter Radio Science Experiment Ice Penetrating Radar Visible-Infrared Hyperspectral Imaging Spectrometer Ultraviolet Imaging Spectrograph Imaging System Magnetometer Particle Package Submillimetre Wave Instrument Radio and Plasma Wave Instrument Overall mission profile 06/2022 - Launch by Ariane-5 ECA + EVEE Cruise 01/2030 - Jupiter orbit insertion Jupiter tour Transfer to Callisto (11 months) Europa phase: 2 Europa and 3 Callisto flybys (1 month) Jupiter High Latitude Phase: 9 Callisto flybys (9 months) Transfer to Ganymede (11 months) 09/2032 – Ganymede orbit insertion Ganymede tour Elliptical and high altitude circular phases (5 months) Low altitude (500 km) circular orbit (4 months) 06/2033 – End of nominal mission Spacecraft 3-axis stabilised Power: solar panels: ~900 W HGA: ~3 m, body fixed X and Ka bands Downlink ≥ 1.4 Gbit/day High Δv capability (2700 m/s) Radiation tolerance: 50 krad at equipment level Dry mass: ~1800 kg Ground TM stations ESTRAC network Key mission drivers Radiation tolerance and technology Power budget and solar arrays challenges Mass budget Responsibilities ESA: manufacturing, launch, operations of the spacecraft and data archiving PI Teams: science payload provision, operations, and data analysis 3 Foreword The JUICE (JUpiter ICy moon Explorer) mission, selected by ESA in May 2012 to be the first large mission within the Cosmic Vision Program 2015–2025, will provide the most comprehensive exploration to date of the Jovian system in all its complexity, with particular emphasis on Ganymede as a planetary body and potential habitat. -
Space Launch System (Sls) Motors
Propulsion Products Catalog SPACE LAUNCH SYSTEM (SLS) MOTORS For NASA’s Space Launch System (SLS), Northrop Grumman manufactures the five-segment SLS heavy- lift boosters, the booster separation motors (BSM), and the Launch Abort System’s (LAS) launch abort motor and attitude control motor. The SLS five-segment booster is the largest solid rocket motor ever built for flight. The SLS booster shares some design heritage with flight-proven four-segment space shuttle reusable solid rocket motors (RSRM), but generates 20 percent greater average thrust and 24 percent greater total impulse. While space shuttle RSRM production has ended, sustained booster production for SLS helps provide cost savings and access to reliable material sources. Designed to push the spent RSRMs safely away from the space shuttle, Northrop Grumman BSMs were rigorously qualified for human space flight and successfully used on the last fifteen space shuttle missions. These same motors are a critical part of NASA’s SLS. Four BSMs are installed in the forward frustum of each five-segment booster and four are installed in the aft skirt, for a total of 16 BSMs per launch. The launch abort motor is an integral part of NASA’s LAS. The LAS is designed to safely pull the Orion crew module away from the SLS launch vehicle in the event of an emergency on the launch pad or during ascent. Northrop Grumman is on contract to Lockheed Martin to build the abort motor and attitude control motor—Lockheed is the prime contractor for building the Orion Multi-Purpose Crew Vehicle designed for use on NASA’s SLS. -
Mars Exploration: an Overview of Indian and International Mars Missions Nayamavalsa Scariah1, Dr
Taurian Innovative Journal/Volume 1/ Issue 1 Mars exploration: An overview of Indian and International Mars Missions NayamaValsa Scariah1, Dr. Mili Ghosh2, Dr.A.P.Krishna3 Birla Institute of Technology, Mesra, Ranchi Abstract- Mars is the fourth planet from the sun. It is 1. Introduction also known as red planet because of its iron oxide content. There are lots of missions have been launched to Mars is also known as red planet, because of the mars for better understanding of our neighboring planet. reddish iron oxide prevalent on its surface gives it a There are lots of unmanned spacecraft including reddish appearance. It is the fourth planet from sun. orbiters, landers and rovers have been launched into mars since early 1960. Sputnik was the first satellite The term sol is used to define duration of solar day on launched in 1957 by Soviet Union. After seven failure Mars. A mean Martian solar day or sol is 24 hours 39 missions to Mars, Mariner 4 was the first satellite which minutes and 34.244 seconds. Many space missions to reached the Martian orbiter successfully. The Viking 1 Mars have been planned and launched for Mars was the first lander reached on Mars on 1975. India exploration (Table:1) but most of them failed without successfully launched a spacecraft, Mangalyan (Mars completing the task specially in early attempts th Orbiter Mission) on 5 November, 2013, with five whereas some NASA missions were very payloads to Mars. India was the first nation to successful(such as the twin Mars Exploration Rovers, successfully reach Mars on its first attempt. -
Constellation Program Overview
Constellation Program Overview October 2008 hris Culbert anager, Lunar Surface Systems Project Office ASA/Johnson Space Center Constellation Program EarthEarth DepartureDeparture OrionOrion -- StageStage CrewCrew ExplorationExploration VehicleVehicle AresAres VV -- HeavyHeavy LiftLift LaunchLaunch VehicleVehicle AltairAltair LunarLunar LanderLander AresAres II -- CrewCrew LaunchLaunch VehicleVehicle Lunar Capabilities Concept Review EstablishedEstablished Lunar Lunar Transportation Transportation EstablishEstablish Lunar Lunar Surface SurfaceArchitecturesArchitectures ArchitectureArchitecture Point Point of of Departure: Departure: StrategiesStrategies which: which: Satisfy NASA NGO’s to acceptable degree ProvidesProvides crew crew & & cargo cargo delivery delivery to to & & from from the the Satisfy NASA NGO’s to acceptable degree within acceptable schedule moonmoon within acceptable schedule Are consistent with capacity and capabilities ProvidesProvides capacity capacity and and ca capabilitiespabilities consistent consistent Are consistent with capacity and capabilities withwith candidate candidate surface surface architectures architectures ofof the the transportation transportation systems systems ProvidesProvides sufficient sufficient performance performance margins margins IncludeInclude set set of of options options fo for rvarious various prioritizations prioritizations of cost, schedule & risk RemainsRemains within within programmatic programmatic constraints constraints of cost, schedule & risk ResultsResults in in acceptable -
Paper Session IA-Shuttle-C Heavy-Lift Vehicle of the 90'S
The Space Congress® Proceedings 1989 (26th) Space - The New Generation Apr 25th, 2:00 PM Paper Session I-A - Shuttle-C Heavy-Lift Vehicle of the 90's Robert G. Eudy Manager, Shuttle-C Task Team, Marshall Space Flight Center Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Eudy, Robert G., "Paper Session I-A - Shuttle-C Heavy-Lift Vehicle of the 90's" (1989). The Space Congress® Proceedings. 5. https://commons.erau.edu/space-congress-proceedings/proceedings-1989-26th/april-25-1989/5 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress® Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. SHUTTLE-C HEAVY-LIFT VEHICLE OF THE 90 ' S Mr. Robert G. Eudy, Manager Shuttle-C Task Team Marshall Space Flight Center ABSTRACT United States current and planned space activities identify the need for increased payload capacity and unmanned flight to complement the existing Shuttle. To meet this challenge the National Aeronautics and Space Administration is defining an unmanned cargo version of the Shuttle that can give the nation early heavy-lift capability. Called Shuttle-C, this unmanned vehicle is a natural, low-cost evolution of the current Space Shuttle that can be flying 100,000 to 170,000 pound payloads by late 1994. At the core of Shuttle-C design philosophy is the principle of evolvement from the United State's Space Transportation System. -
Why NASA's Planet-Hunting Astrophysics Telescope Is an Easy Budget Target, and What Defeat Would Mean PAGE 24
Q & A 12 ASTRONAUT’S VIEW 20 SPACE LAUNCH 34 Neil deGrasse Tyson A realistic moon plan SLS versus commercial SPECIAL REPORT SPACE DARK ENERGY DILEMMA Why NASA’s planet-hunting astrophysics telescope is an easy budget target, and what defeat would mean PAGE 24 APRIL 2018 | A publication of the American Institute of Aeronautics andd Astronautics | aeroaerospaceamerica.aiaa.orgerospaceamerica.aiaa.org 9–11 JULY 2018 CINCINNATI, OH ANNOUNCING EXPANDED TECHNICAL CONTENT FOR 2018! You already know about our extensive technical paper presentations, but did you know that we are now offering an expanded educational program as part of the AIAA Propulsion and Energy Forum and Exposition? In addition to our pre-forum short courses and workshops, we’ve enhanced the technical panels and added focused technical tutorials, high level discussion groups, exciting keynotes and more. LEARN MORE AND REGISTER TODAY! For complete program details please visit: propulsionenergy.aiaa.org FEATURES | April 2018 MORE AT aerospaceamerica.aiaa.org 20 34 40 24 Returning to Launching the Laying down the What next the moon Europa Clipper rules for space Senior research scientist NASA, Congress and We asked experts in for WFIRST? and former astronaut the White House are space policy to comment Tom Jones writes about debating which rocket on proposed United NASA’s three upcoming space what it would take to should send the probe Nations guidelines deliver the funds and into orbit close to this for countries and telescopes are meant to piece together political support for the Jovian moon. companies sending some heady puzzles, but the White Lunar Orbital Outpost- satellites and other craft House’s 2019 budget proposal would Gateway. -
Atlas Launch System Mission Planner's Guide, Atlas V Addendum
ATLAS Atlas Launch System Mission Planner’s Guide, Atlas V Addendum FOREWORD This Atlas V Addendum supplements the current version of the Atlas Launch System Mission Plan- ner’s Guide (AMPG) and presents the initial vehicle capabilities for the newly available Atlas V launch system. Atlas V’s multiple vehicle configurations and performance levels can provide the optimum match for a range of customer requirements at the lowest cost. The performance data are presented in sufficient detail for preliminary assessment of the Atlas V vehicle family for your missions. This guide, in combination with the AMPG, includes essential technical and programmatic data for preliminary mission planning and spacecraft design. Interface data are in sufficient detail to assess a first-order compatibility. This guide contains current information on Lockheed Martin’s plans for Atlas V launch services. It is subject to change as Atlas V development progresses, and will be revised peri- odically. Potential users of Atlas V launch service are encouraged to contact the offices listed below to obtain the latest technical and program status information for the Atlas V development. For technical and business development inquiries, contact: COMMERCIAL BUSINESS U.S. GOVERNMENT INQUIRIES BUSINESS INQUIRIES Telephone: (691) 645-6400 Telephone: (303) 977-5250 Fax: (619) 645-6500 Fax: (303) 971-2472 Postal Address: Postal Address: International Launch Services, Inc. Commercial Launch Services, Inc. P.O. Box 124670 P.O. Box 179 San Diego, CA 92112-4670 Denver, CO 80201 Street Address: Street Address: International Launch Services, Inc. Commercial Launch Services, Inc. 101 West Broadway P.O. Box 179 Suite 2000 MS DC1400 San Diego, CA 92101 12999 Deer Creek Canyon Road Littleton, CO 80127-5146 A current version of this document can be found, in electronic form, on the Internet at: http://www.ilslaunch.com ii ATLAS LAUNCH SYSTEM MISSION PLANNER’S GUIDE ATLAS V ADDENDUM (AVMPG) REVISIONS Revision Date Rev No. -
Atlas V Cutaway Poster
ATLAS V Since 2002, Atlas V rockets have delivered vital national security, science and exploration, and commercial missions for customers across the globe including the U.S. Air Force, the National Reconnaissance Oice and NASA. 225 ft The spacecraft is encapsulated in either a 5-m (17.8-ft) or a 4-m (13.8-ft) diameter payload fairing (PLF). The 4-m-diameter PLF is a bisector (two-piece shell) fairing consisting of aluminum skin/stringer construction with vertical split-line longerons. The Atlas V 400 series oers three payload fairing options: the large (LPF, shown at left), the extended (EPF) and the extra extended (XPF). The 5-m PLF is a sandwich composite structure made with a vented aluminum-honeycomb core and graphite-epoxy face sheets. The bisector (two-piece shell) PLF encapsulates both the Centaur upper stage and the spacecraft, which separates using a debris-free pyrotechnic actuating 200 ft system. Payload clearance and vehicle structural stability are enhanced by the all-aluminum forward load reactor (FLR), which centers the PLF around the Centaur upper stage and shares payload shear loading. The Atlas V 500 series oers 1 three payload fairing options: the short (shown at left), medium 18 and long. 1 1 The Centaur upper stage is 3.1 m (10 ft) in diameter and 12.7 m (41.6 ft) long. Its propellant tanks are constructed of pressure-stabilized, corrosion-resistant stainless steel. Centaur is a liquid hydrogen/liquid oxygen-fueled vehicle. It uses a single RL10 engine producing 99.2 kN (22,300 lbf) of thrust. -
Space Solutions Fact Sheet
www.dynetics. Space Solutions Fact Sheet The Space Division at Dynetics, Inc., headquartered Key Facts in Huntsville, Ala., provides flexible flight hardware ▪ Building a Human Landing System (HLS) for NASA’s development from low-cost prototypes through Artemis program complete human-rated solutions. ▪ NASA contractor for Space Launch System’s (SLS) Universal Stage Adapter (USA) Dynetics Space Division’s capabilities include ▪ NASA Glenn Research Center’s Large Business Prime propulsion systems, small satellite development, Contractor of the Year (2018) mechanical and propulsion testing, system ▪ Lonestar Small Satellite Developer for SMDC integration and assembly, mission design and ▪ Propulsion system provider for Astrobotic robotic lunar vehicle sizing and vehicle structure design and lander manufacturing. ▪ Developer of innovative spacecraft and missile propulsion systems About Dynetics ▪ Built the NASA Space Launch System’s Core Stage Pathfinder Dynetics, a wholly owned subsidiary of Leidos, ▪ Designed the Laser Air Monitoring System (LAMS) for provides responsive, cost-effective engineering, NASA Orion program scientific, IT solutions to the national security, ▪ Prime contractor for NASA SLS Advanced Booster cybersecurity, space, and critical infrastructure Engineering Demonstration and Risk Reduction (ABEDRR) sectors. Our portfolio features highly specialized demonstrated low-cost, full-scale cryogenic tank technical services and a range of software and ▪ Provider of critical flight components for SLS Core Stage hardware products, including components, and SLS Exploration Upper Stage ▪ Certified to build NASA, DoD, and commercial flight subsystems, and complex end-to-end systems. hardware The company of more than 3,000 employees ▪ More than 500,000 sq. feet of research and development is based in Huntsville, Ala., and has offices facilities in North Alabama throughout the U.S.