Mars Landing
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Flight Opportunities and Small Spacecraft Technology Program Updates NAC Technology, Innovation and Engineering Committee Meeting | March 19, 2020
Flight Opportunities and Small Spacecraft Technology Program Updates NAC Technology, Innovation and Engineering Committee Meeting | March 19, 2020 Christopher Baker NASA Space Technology Mission Directorate Flight Opportunities and Small Spacecraft Technology Program Executive National Aeronautics and Space Administration 1 CHANGING THE PACE OF SPACE Through Small Spacecraft Technology and Flight Opportunities, Space Tech is pursuing the rapid identification, development, and testing of capabilities that exploit agile spacecraft platforms and responsive launch capabilities to increase the pace of space exploration, discovery, and the expansion of space commerce. National Aeronautics and Space Administration 2 THROUGH SUBORBITAL FLIGHT The Flight Opportunities program facilitates rapid demonstration of promising technologies for space exploration, discovery, and the expansion of space commerce through suborbital testing with industry flight providers LEARN MORE: WWW.NASA.GOV/TECHNOLOGY Photo Credit: Blue Origin National Aeronautics and Space Administration 3 FLIGHT OPPORTUNITIES BY THE NUMBERS Between 2011 and today… In 2019 alone… Supported 195 successful fights Supported 15 successful fights Enabled 676 tests of payloads Enabled 47 tests of payloads 254 technologies in the portfolio 86 technologies in the portfolio 13 active commercial providers 9 active commercial providers National Aeronautics and Space Administration Numbers current as of March 1, 2020 4 TECHNOLOGY TESTED IN SUBORBITAL Lunar Payloads ISS SPACE IS GOING TO EARTH ORBIT, THE MOON, MARS, AND BEYOND Mars 2020 Commercial Critical Space Lunar Payload Exploration Services Solutions National Aeronautics and Space Administration 5 SUBORBITAL INFUSION HIGHLIGHT Commercial Lunar Payload Services Four companies selected as Commercial Lunar Payload Services (CPLS) providers leveraged Flight Opportunities-supported suborbital flights to test technologies that are incorporated into their landers and/or are testing lunar landing technologies under Flight Opportunities for others. -
Tianwen-1: China's Mars Mission
Tianwen-1: China's Mars Mission drishtiias.com/printpdf/tianwen-1-china-s-mars-mission Why In News China will launch its first Mars Mission - Tianwen-1- in July, 2020. China's previous ‘Yinghuo-1’ Mars mission, which was supported by a Russian spacecraft, had failed after it did not leave the earth's orbit and disintegrated over the Pacific Ocean in 2012. The National Aeronautics and Space Administration (NASA) is also going to launch its own Mars mission in July, the Perseverance which aims to collect Martian samples. Key Points The Tianwen-1 Mission: It will lift off on a Long March 5 rocket, from the Wenchang launch centre. It will carry 13 payloads (seven orbiters and six rovers) that will explore the planet. It is an all-in-one orbiter, lander and rover system. Orbiter: It is a spacecraft designed to orbit a celestial body (astronomical body) without landing on its surface. Lander: It is a strong, lightweight spacecraft structure, consisting of a base and three sides "petals" in the shape of a tetrahedron (pyramid- shaped). It is a protective "shell" that houses the rover and protects it, along with the airbags, from the forces of impact. Rover: It is a planetary surface exploration device designed to move across the solid surface on a planet or other planetary mass celestial bodies. 1/3 Objectives: The mission will be the first to place a ground-penetrating radar on the Martian surface, which will be able to study local geology, as well as rock, ice, and dirt distribution. It will search the martian surface for water, investigate soil characteristics, and study the atmosphere. -
Appendix 1: Venus Missions
Appendix 1: Venus Missions Sputnik 7 (USSR) Launch 02/04/1961 First attempted Venus atmosphere craft; upper stage failed to leave Earth orbit Venera 1 (USSR) Launch 02/12/1961 First attempted flyby; contact lost en route Mariner 1 (US) Launch 07/22/1961 Attempted flyby; launch failure Sputnik 19 (USSR) Launch 08/25/1962 Attempted flyby, stranded in Earth orbit Mariner 2 (US) Launch 08/27/1962 First successful Venus flyby Sputnik 20 (USSR) Launch 09/01/1962 Attempted flyby, upper stage failure Sputnik 21 (USSR) Launch 09/12/1962 Attempted flyby, upper stage failure Cosmos 21 (USSR) Launch 11/11/1963 Possible Venera engineering test flight or attempted flyby Venera 1964A (USSR) Launch 02/19/1964 Attempted flyby, launch failure Venera 1964B (USSR) Launch 03/01/1964 Attempted flyby, launch failure Cosmos 27 (USSR) Launch 03/27/1964 Attempted flyby, upper stage failure Zond 1 (USSR) Launch 04/02/1964 Venus flyby, contact lost May 14; flyby July 14 Venera 2 (USSR) Launch 11/12/1965 Venus flyby, contact lost en route Venera 3 (USSR) Launch 11/16/1965 Venus lander, contact lost en route, first Venus impact March 1, 1966 Cosmos 96 (USSR) Launch 11/23/1965 Possible attempted landing, craft fragmented in Earth orbit Venera 1965A (USSR) Launch 11/23/1965 Flyby attempt (launch failure) Venera 4 (USSR) Launch 06/12/1967 Successful atmospheric probe, arrived at Venus 10/18/1967 Mariner 5 (US) Launch 06/14/1967 Successful flyby 10/19/1967 Cosmos 167 (USSR) Launch 06/17/1967 Attempted atmospheric probe, stranded in Earth orbit Venera 5 (USSR) Launch 01/05/1969 Returned atmospheric data for 53 min on 05/16/1969 M. -
Status of the Space Shuttle Solid Rocket Booster
The Space Congress® Proceedings 1980 (17th) A New Era In Technology Apr 1st, 8:00 AM Status of The Space Shuttle Solid Rocket Booster William P. Horton Solid Rocket Booster Engineering Office, George C. Marshall Space Flight Center, Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Horton, William P., "Status of The Space Shuttle Solid Rocket Booster" (1980). The Space Congress® Proceedings. 3. https://commons.erau.edu/space-congress-proceedings/proceedings-1980-17th/session-1/3 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]. STATUS OF THE SPACE SHUTTLE SOLID ROCKET BOOSTER William P. Horton, Chief Engineer Solid Rocket Booster Engineering Office George C. Marshall Space Flight Center, AL 35812 ABSTRACT discuss retrieval and refurbishment plans for Booster reuse, and will address Booster status Two Solid Rocket Boosters provide the primary for multimission use. first stage thrust for the Space Shuttle. These Boosters, the largest and most powerful solid rocket vehicles to meet established man- BOOSTER CONFIGURATION rated design criteria, are unique in that they are also designed to be recovered, refurbished, It is appropriate to review the Booster config and reused. uration before describing the mission profile. The Booster is 150 feet long and is 148 inches The first SRB f s have been stacked on the in diameter (Figure 1), The inert weight Mobile Launch Platform at the Kennedy Space is 186,000 pounds and the propellant weight is Center and are ready to be mated with the approximately 1.1 million pounds for each External Tank and Orbiter in preparation for Booster. -
Design a Crew Module Drop Test Data Log Use This Data Log to Record the Results of Each Drop Test
National Aeronautics and DESIGN A Space Administration CREWYour Challenge MODULE Design and build a crew module model that will secure two astronaut figures during a drop test. Do First Watch the instructional video for this module: go.nasa.gov/34hVUvL Astronaut safety is of the highest Design Constraints importance. For Artemis missions, 1) The crew module must safely carry two astronauts. You must design and build a secure NASA’s Orion spacecraft must seat for the astronauts, without gluing or taping them in place. The astronauts should be able to support astronauts stay in their seats during each drop test. for weeks at a time and operate reliably in the harsh space 2) The crew module must fit into the container you chose. This item is simply for size environment. restraints. The crew module must not be dropped while inside the container. 3) The crew module must have one hatch that opens and closes easily. The hatch should remain shut during all drop tests. 4) Your crew module design should consider mass and strength. Mass is important in space travel. The heavier the crew module, the more expensive it is to build and, ultimately, to launch. NASA is looking for a lightweight but strong crew module. Ask and Imagine Think of ways to safely secure two astronauts inside of the crew module. Learn more: • What types of materials will protect the astronauts? Orion Capabilities for Deep Space • How can you reduce the impact on the crew module and astronauts? Enabled Crewed Artemis Moon • What essential elements are needed for crew safety? Missions go.nasa.gov/2GEMBN1 Top 5 Technologies needed for a LET’S GET STARTED! Spacecraft to Survive Deep Space 1. -
O'keefe Resigns
Volume 46 Issue 11 Dryden Flight Research Center, Edwards, California December 31, 2004 O’Keefe resigns NASA News Services FondFondFond NASAAdministrator Sean O’Keefe, who in the past three years led the Agency through an aggressive and comprehensive management transformation and helped it through one of its most painful tragedies, has resigned his post. In his resignation letter to President Bush, O’Keefe wrote, “I will continue until you have named a successor and in the hope the Senate will act on your nomination by February.” FarewellFarewellFarewell “I’ve been honored to serve this ■ Storied research aircraft president, the American people and my retired after more than talented colleagues here at NASA,” four decades in the skies O’Keefe said. “Together, we’ve enjoyed unprecedented success and By Jay Levine seen each other through arduous X-Press Editor circumstances. This was the most Dryden’s venerable NB-52B aircraft difficult decision I’ve ever made, but was recognized Dec. 17 for a career it’s one I felt was best for my family spanning nearly fifty years, a tour of duty and our future.” in which the big bird played a role in O’Keefe, 48, is NASA’s 10th airlaunching generations of experimental administrator. Nominated by President aircraft. Bush and confirmed by the U.S. The retirement ceremony brought Senate, he was sworn into office Dec. together people from the aircraft’s past 21, 2001. It was O’Keefe’s fourth and present as it is prepared for its future presidential appointment. as a historical monument at the Edwards Air After joining NASA, O’Keefe Force Base north gate. -
Nasa's Commercial Crew Development
NASA’S COMMERCIAL CREW DEVELOPMENT PROGRAM: ACCOMPLISHMENTS AND CHALLENGES HEARING BEFORE THE COMMITTEE ON SCIENCE, SPACE, AND TECHNOLOGY HOUSE OF REPRESENTATIVES ONE HUNDRED TWELFTH CONGRESS FIRST SESSION WEDNESDAY, OCTOBER 26, 2011 Serial No. 112–46 Printed for the use of the Committee on Science, Space, and Technology ( Available via the World Wide Web: http://science.house.gov U.S. GOVERNMENT PRINTING OFFICE 70–800PDF WASHINGTON : 2011 For sale by the Superintendent of Documents, U.S. Government Printing Office Internet: bookstore.gpo.gov Phone: toll free (866) 512–1800; DC area (202) 512–1800 Fax: (202) 512–2104 Mail: Stop IDCC, Washington, DC 20402–0001 COMMITTEE ON SCIENCE, SPACE, AND TECHNOLOGY HON. RALPH M. HALL, Texas, Chair F. JAMES SENSENBRENNER, JR., EDDIE BERNICE JOHNSON, Texas Wisconsin JERRY F. COSTELLO, Illinois LAMAR S. SMITH, Texas LYNN C. WOOLSEY, California DANA ROHRABACHER, California ZOE LOFGREN, California ROSCOE G. BARTLETT, Maryland BRAD MILLER, North Carolina FRANK D. LUCAS, Oklahoma DANIEL LIPINSKI, Illinois JUDY BIGGERT, Illinois GABRIELLE GIFFORDS, Arizona W. TODD AKIN, Missouri DONNA F. EDWARDS, Maryland RANDY NEUGEBAUER, Texas MARCIA L. FUDGE, Ohio MICHAEL T. MCCAUL, Texas BEN R. LUJA´ N, New Mexico PAUL C. BROUN, Georgia PAUL D. TONKO, New York SANDY ADAMS, Florida JERRY MCNERNEY, California BENJAMIN QUAYLE, Arizona JOHN P. SARBANES, Maryland CHARLES J. ‘‘CHUCK’’ FLEISCHMANN, TERRI A. SEWELL, Alabama Tennessee FREDERICA S. WILSON, Florida E. SCOTT RIGELL, Virginia HANSEN CLARKE, Michigan STEVEN M. PALAZZO, Mississippi VACANCY MO BROOKS, Alabama ANDY HARRIS, Maryland RANDY HULTGREN, Illinois CHIP CRAVAACK, Minnesota LARRY BUCSHON, Indiana DAN BENISHEK, Michigan VACANCY (II) C O N T E N T S Wednesday, October 26, 2011 Page Witness List ............................................................................................................ -
Mars Insight Launch Press Kit
Introduction National Aeronautics and Space Administration Mars InSight Launch Press Kit MAY 2018 www.nasa.gov 1 2 Table of Contents Table of Contents Introduction 4 Media Services 8 Quick Facts: Launch Facts 12 Quick Facts: Mars at a Glance 16 Mission: Overview 18 Mission: Spacecraft 30 Mission: Science 40 Mission: Landing Site 53 Program & Project Management 55 Appendix: Mars Cube One Tech Demo 56 Appendix: Gallery 60 Appendix: Science Objectives, Quantified 62 Appendix: Historical Mars Missions 63 Appendix: NASA’s Discovery Program 65 3 Introduction Mars InSight Launch Press Kit Introduction NASA’s next mission to Mars -- InSight -- will launch from Vandenberg Air Force Base in California as early as May 5, 2018. It is expected to land on the Red Planet on Nov. 26, 2018. InSight is a mission to Mars, but it is more than a Mars mission. It will help scientists understand the formation and early evolution of all rocky planets, including Earth. A technology demonstration called Mars Cube One (MarCO) will share the launch with InSight and fly separately to Mars. Six Ways InSight Is Different NASA has a long and successful track record at Mars. Since 1965, it has flown by, orbited, landed and roved across the surface of the Red Planet. None of that has been easy. Only about 40 percent of the missions ever sent to Mars by any space agency have been successful. The planet’s thin atmosphere makes landing a challenge; its extreme temperature swings make it difficult to operate on the surface. But if a spacecraft survives the trip, there’s a bounty of science to be collected. -
K.Klaus, M. L. Raftery and K. E. Post, the Boeing Company, 13100 Space Center Blvd, Houston TX 77059 [email protected], Mi
An Affordable Mars Mission Design K.Klaus, M. L. Raftery and K. E. Post, The Boeing Company, 13100 Space Center Blvd, Houston TX 77059 [email protected], [email protected], [email protected]. Introduction: The International goal of sending human explorers to Mars. Key ndings of a 2013 Humans to Mars ultimately represent a risk to the human Mars landing objective. Strategic knowledge Mars Sample Return Mission MAV Derived space community has declared that conference panel discussion on mission architectures were; 1) A human mission to gaps for human missions to Mars have been studied by various groups, most recently Concept: Mars sample return (MSR) is Lunar Lander our unied long term goal is for a Mars is on the same order of magnitude as the effort it took to build the International the Mars Exploration Program Analysis Group (MEPAG).[4] For the life support and one of the highest priorities of the human mission to Mars but major Space Station (ISS); a substantial effort but one that is likely affordable in the current crew accommodation equipment, the ISS can be used to reduce risk for the Mars Science Mission Directorate at NASA. work remains to dene how it will be budget environment; 2) An inclusive, international process should be used to establish mission. Subsystem equipment can also be tested on ISS, but ultimately, human [6] As a stepping stone to Mars, the done. We will describe a “stepping the exploration objectives and dene the experience in the deep space MSR mission could provide valuable stone” based approach that charts a capabilities that are needed to achieve environment is needed. -
A Review of Sample Analysis at Mars-Evolved Gas Analysis Laboratory Analog Work Supporting the Presence of Perchlorates and Chlorates in Gale Crater, Mars
minerals Review A Review of Sample Analysis at Mars-Evolved Gas Analysis Laboratory Analog Work Supporting the Presence of Perchlorates and Chlorates in Gale Crater, Mars Joanna Clark 1,* , Brad Sutter 2, P. Douglas Archer Jr. 2, Douglas Ming 3, Elizabeth Rampe 3, Amy McAdam 4, Rafael Navarro-González 5,† , Jennifer Eigenbrode 4 , Daniel Glavin 4 , Maria-Paz Zorzano 6,7 , Javier Martin-Torres 7,8, Richard Morris 3, Valerie Tu 2, S. J. Ralston 2 and Paul Mahaffy 4 1 GeoControls Systems Inc—Jacobs JETS Contract at NASA Johnson Space Center, Houston, TX 77058, USA 2 Jacobs JETS Contract at NASA Johnson Space Center, Houston, TX 77058, USA; [email protected] (B.S.); [email protected] (P.D.A.J.); [email protected] (V.T.); [email protected] (S.J.R.) 3 NASA Johnson Space Center, Houston, TX 77058, USA; [email protected] (D.M.); [email protected] (E.R.); [email protected] (R.M.) 4 NASA Goddard Space Flight Center, Greenbelt, MD 20771, USA; [email protected] (A.M.); [email protected] (J.E.); [email protected] (D.G.); [email protected] (P.M.) 5 Institito de Ciencias Nucleares, Universidad Nacional Autonoma de Mexico, Mexico City 04510, Mexico; [email protected] 6 Centro de Astrobiología (INTA-CSIC), Torrejon de Ardoz, 28850 Madrid, Spain; [email protected] 7 Department of Planetary Sciences, School of Geosciences, University of Aberdeen, Aberdeen AB24 3FX, UK; [email protected] 8 Instituto Andaluz de Ciencias de la Tierra (CSIC-UGR), Armilla, 18100 Granada, Spain Citation: Clark, J.; Sutter, B.; Archer, * Correspondence: [email protected] P.D., Jr.; Ming, D.; Rampe, E.; † Deceased 28 January 2021. -
Low Velocity Airdrop Tests of an X-38 Backup Parachute Design
Source of Acquisition NASA Johnson Space Center Low Velocity Airdrop Tests of an X-38 Backup Parachute Design Jenny M. stein* and Ricardo A. ~achin~ NASA Johnson Space Center, Houston, Texas, 77059 Dean F. wolft. Albz~querque,New Mexico, 871 11 and F. David ~illebrandt~ United Space Alliance, Kennedy Space Center, Florida, 32815 The NASA Johnson Space Center's X-38 program designed a new backup parachute system to recover the 25,000 lb X-38 prototype for the Crew Return Vehicle spacecraft. Due to weight and cost constraints, the main backup parachute design incorporated rapid and low cost fabrication techniques using off-the-shelf materials. Near the vent, the canopy was constructed of continuous ribbons, to provide more damage tolerance. The remainder of the canopy was a constructed with a continuous ringslot design. After cancellation of the X-38 program, the parachute design was resized, built, and drop tested for Natick Soldiers Center's Low Velocity Air Drop (LVAD) program to deliver cargo loads up to 22,000 Ibs from altitudes as low as 500 feet above the ground. Drop tests results showed that the 500- foot LVAD parachute deployment conditions cause severe skirt inversion and inflation problems for large parachutes. The bag strip occurred at a high angle of attack, causing skirt inversion before the parachute could inflate. The addition of a short reefing line prevented the skirt inversion. Using a lower porosity in the vent area, than is normally used in large parachutes, improved inflation. The drop testing demonstrated that the parachute design could be refined to meet the requirements for the 500-foot LVAD mission. -
Launch Abort System Crew Module Service Module
LAUNCH ABORT SYSTEM National Aeronautics and The launch abort system, positioned on a tower atop the Space Administration crew module, can activate within milliseconds to propel the vehicle to safety and position the crew module for a safe landing. CREW MODULE The crew module is capable of transporting four to six crew members beyond the moon, providing a safe habitat from launch through landing and recovery. Inside the familiar deep-space capsule shape are advances in life support, avionics, power systems, and advanced manufacturing techniques. SERVICE MODULE Created in collaboration with ESA (European Space Agency), the service module provides support to the crew module from launch through separation prior to entry. It NASA’s Orion spacecraft will carry astronauts provides in-space propulsion capability for orbital transfer, farther than humans have ever gone before. attitude control and high altitude ascent aborts. While It will serve as the exploration vehicle that will mated with the crew module, it also provides water and air carry the crew to deep space, provide to support the crew. emergency abort capability, sustain astronauts during their missions and provide safe re-entry SPACE LAUNCH SYSTEM back to Earth. The Space Launch System is a powerful launch vehicle, which will expand human presence to celestial destinations beyond low-Earth orbit and throughout the Orion features technology advancements and solar system. This launch vehicle will be capable of innovations that have been incorporated into launching Orion to asteroids, the moon and on the the spacecraft's design. It includes crew and journey to Mars. service modules, a spacecraft adapter and a revolutionary launch abort system that will significantly increase crew safety.