Space Flight and Its Types
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The Space Launch System for Exploration and Science. K
45th Lunar and Planetary Science Conference (2014) 2234.pdf THE SPACE LAUNCH SYSTEM FOR EXPLORATION AND SCIENCE. K. Klaus1, M. S. Elsperman1, B. B. Donahue1, K. E. Post1, M. L. Raftery1, and D. B. Smith1, 1The Boeing Company, 13100 Space Center Blvd, Houston TX 77059, [email protected], [email protected], [email protected], mi- [email protected], [email protected], [email protected]. Introduction: The Space Launch System (SLS) is same time which will simplify mission design and re- the most powerful rocket ever built and provides a duce launch costs. One of the key features of the SLS critical heavy-lift launch capability enabling diverse in cislunar space is performance to provide “dual-use”, deep space missions. This exploration class vehicle i.e. Orion plus 15t of any other payload. launches larger payloads farther in our solar system An opportunity exists to deliver payload to the lu- and faster than ever before. Available fairing diameters nar surface or lunar orbit on the unmanned 2017 range from 5 m to 10 m; these allow utilization of ex- MPCV/ SLS test flight (~4.5t of mass margin exists for isting systems which reduces development risks, size this flight). Concepts of this nature can be done for limitations and cost. SLS injection capacity shortens less than Discovery class mission budgets (~$450M) mission travel time. Enhanced capabilities enable a and may be done as a joint venture by the NASA Sci- variety of missions including human exploration, plan- ence Mission Directorate and Human Exploration Op- etary science, astrophysics, heliophysics, planetary erations Mission Directorate using the successful Lu- defense, Earth observaton and commercial space en- nar Reconnaissance Orbiter as a program model. -
Electric Propulsion System Scaling for Asteroid Capture-And-Return Missions
Electric propulsion system scaling for asteroid capture-and-return missions Justin M. Little⇤ and Edgar Y. Choueiri† Electric Propulsion and Plasma Dynamics Laboratory, Princeton University, Princeton, NJ, 08544 The requirements for an electric propulsion system needed to maximize the return mass of asteroid capture-and-return (ACR) missions are investigated in detail. An analytical model is presented for the mission time and mass balance of an ACR mission based on the propellant requirements of each mission phase. Edelbaum’s approximation is used for the Earth-escape phase. The asteroid rendezvous and return phases of the mission are modeled as a low-thrust optimal control problem with a lunar assist. The numerical solution to this problem is used to derive scaling laws for the propellant requirements based on the maneuver time, asteroid orbit, and propulsion system parameters. Constraining the rendezvous and return phases by the synodic period of the target asteroid, a semi- empirical equation is obtained for the optimum specific impulse and power supply. It was found analytically that the optimum power supply is one such that the mass of the propulsion system and power supply are approximately equal to the total mass of propellant used during the entire mission. Finally, it is shown that ACR missions, in general, are optimized using propulsion systems capable of processing 100 kW – 1 MW of power with specific impulses in the range 5,000 – 10,000 s, and have the potential to return asteroids on the order of 103 104 tons. − Nomenclature -
AFSPC-CO TERMINOLOGY Revised: 12 Jan 2019
AFSPC-CO TERMINOLOGY Revised: 12 Jan 2019 Term Description AEHF Advanced Extremely High Frequency AFB / AFS Air Force Base / Air Force Station AOC Air Operations Center AOI Area of Interest The point in the orbit of a heavenly body, specifically the moon, or of a man-made satellite Apogee at which it is farthest from the earth. Even CAP rockets experience apogee. Either of two points in an eccentric orbit, one (higher apsis) farthest from the center of Apsis attraction, the other (lower apsis) nearest to the center of attraction Argument of Perigee the angle in a satellites' orbit plane that is measured from the Ascending Node to the (ω) perigee along the satellite direction of travel CGO Company Grade Officer CLV Calculated Load Value, Crew Launch Vehicle COP Common Operating Picture DCO Defensive Cyber Operations DHS Department of Homeland Security DoD Department of Defense DOP Dilution of Precision Defense Satellite Communications Systems - wideband communications spacecraft for DSCS the USAF DSP Defense Satellite Program or Defense Support Program - "Eyes in the Sky" EHF Extremely High Frequency (30-300 GHz; 1mm-1cm) ELF Extremely Low Frequency (3-30 Hz; 100,000km-10,000km) EMS Electromagnetic Spectrum Equitorial Plane the plane passing through the equator EWR Early Warning Radar and Electromagnetic Wave Resistivity GBR Ground-Based Radar and Global Broadband Roaming GBS Global Broadcast Service GEO Geosynchronous Earth Orbit or Geostationary Orbit ( ~22,300 miles above Earth) GEODSS Ground-Based Electro-Optical Deep Space Surveillance -
Vostok by Andrew J
Mercury's Competition: Vostok by Andrew J. LePage May 15, 2000 All through 1959 and into 1960, America's very single space suit-clad cosmonaut in a semi reclined public Mercury manned space program was making ejection seat which served a dual purpose: During the slow but steady progress (see Giving Mercury early phases of ascent, this seat could safely eject the Wings in the September 1, 1999 issue of cosmonaut away from the craft in case of a problem. SpaceViews). While it was quite clear that the Soviet Because of weight restrictions, the capsule could not Union also planned to send men into space, it was carry a large enough parachute to guarantee a soft difficult to sort the facts from the stream of enough landing for the pilot at the end of a normal propaganda. That began to change on May 15, 1960 mission. Instead a forced landing procedure was with the launch of Korabl Sputnik 1 (Spaceship developed where, after reentry was done, the Satellite 1) also referred to as "Sputnik 4" in the cosmonaut ejected from the descent module at an West. altitude of 7 kilometers (23,000 feet). He then used his own parachute to make a soft landing separate Carrying a dummy cosmonaut in a 312 by 369 from the more quickly falling descent module. kilometer (194 by 229 mile) orbit inclined 65 degrees to the equator, Korabl Sputnik 1 was the long awaited During the flight, the cabin interior maintained an inaugural flight of Mercury's competition. Although oxygen-nitrogen atmosphere at a pressure of one bar the actual configuration of the spacecraft would (15 psi) like on the ground. -
Breakthrough Propulsion Study Assessing Interstellar Flight Challenges and Prospects
Breakthrough Propulsion Study Assessing Interstellar Flight Challenges and Prospects NASA Grant No. NNX17AE81G First Year Report Prepared by: Marc G. Millis, Jeff Greason, Rhonda Stevenson Tau Zero Foundation Business Office: 1053 East Third Avenue Broomfield, CO 80020 Prepared for: NASA Headquarters, Space Technology Mission Directorate (STMD) and NASA Innovative Advanced Concepts (NIAC) Washington, DC 20546 June 2018 Millis 2018 Grant NNX17AE81G_for_CR.docx pg 1 of 69 ABSTRACT Progress toward developing an evaluation process for interstellar propulsion and power options is described. The goal is to contrast the challenges, mission choices, and emerging prospects for propulsion and power, to identify which prospects might be more advantageous and under what circumstances, and to identify which technology details might have greater impacts. Unlike prior studies, the infrastructure expenses and prospects for breakthrough advances are included. This first year's focus is on determining the key questions to enable the analysis. Accordingly, a work breakdown structure to organize the information and associated list of variables is offered. A flow diagram of the basic analysis is presented, as well as more detailed methods to convert the performance measures of disparate propulsion methods into common measures of energy, mass, time, and power. Other methods for equitable comparisons include evaluating the prospects under the same assumptions of payload, mission trajectory, and available energy. Missions are divided into three eras of readiness (precursors, era of infrastructure, and era of breakthroughs) as a first step before proceeding to include comparisons of technology advancement rates. Final evaluation "figures of merit" are offered. Preliminary lists of mission architectures and propulsion prospects are provided. -
Orbit and Spin
Orbit and Spin Overview: A whole-body activity that explores the relative sizes, distances, orbit, and spin of the Sun, Earth, and Moon. Target Grade Level: 3-5 Estimated Duration: 2 40-minute sessions Learning Goals: Students will be able to… • compare the relative sizes of the Earth, Moon, and Sun. • contrast the distance between the Earth and Moon to the distance between the Earth and Sun. • differentiate between the motions of orbit and spin. • demonstrate the spins of the Earth and the Moon, as well as the orbits of the Earth around the Sun, and the Moon around the Earth. Standards Addressed: Benchmarks (AAAS, 1993) The Physical Setting, 4A: The Universe, 4B: The Earth National Science Education Standards (NRC, 1996) Physical Science, Standard B: Position and motion of objects Earth and Space Science, Standard D: Objects in the sky, Changes in Earth and sky Table of Contents: Background Page 1 Materials and Procedure 5 What I Learned… Science Journal Page 14 Earth Picture 15 Sun Picture 16 Moon Picture 17 Earth Spin Demonstration 18 Moon Orbit Demonstration 19 Extensions and Adaptations 21 Standards Addressed, detailed 22 Background: Sun The Sun is the center of our Solar System, both literally—as all of the planets orbit around it, and figuratively—as its rays warm our planet and sustain life as we know it. The Sun is very hot compared to temperatures we usually encounter. Its mean surface temperature is about 9980° Fahrenheit (5800 Kelvin) and its interior temperature is as high as about 28 million° F (15,500,000 Kelvin). -
+ New Horizons
Media Contacts NASA Headquarters Policy/Program Management Dwayne Brown New Horizons Nuclear Safety (202) 358-1726 [email protected] The Johns Hopkins University Mission Management Applied Physics Laboratory Spacecraft Operations Michael Buckley (240) 228-7536 or (443) 778-7536 [email protected] Southwest Research Institute Principal Investigator Institution Maria Martinez (210) 522-3305 [email protected] NASA Kennedy Space Center Launch Operations George Diller (321) 867-2468 [email protected] Lockheed Martin Space Systems Launch Vehicle Julie Andrews (321) 853-1567 [email protected] International Launch Services Launch Vehicle Fran Slimmer (571) 633-7462 [email protected] NEW HORIZONS Table of Contents Media Services Information ................................................................................................ 2 Quick Facts .............................................................................................................................. 3 Pluto at a Glance ...................................................................................................................... 5 Why Pluto and the Kuiper Belt? The Science of New Horizons ............................... 7 NASA’s New Frontiers Program ........................................................................................14 The Spacecraft ........................................................................................................................15 Science Payload ...............................................................................................................16 -
Solar System Exploration: a Vision for the Next Hundred Years
IAC-04-IAA.3.8.1.02 SOLAR SYSTEM EXPLORATION: A VISION FOR THE NEXT HUNDRED YEARS R. L. McNutt, Jr. Johns Hopkins University Applied Physics Laboratory Laurel, Maryland, USA [email protected] ABSTRACT The current challenge of space travel is multi-tiered. It includes continuing the robotic assay of the solar system while pressing the human frontier beyond cislunar space, with Mars as an ob- vious destination. The primary challenge is propulsion. For human voyages beyond Mars (and perhaps to Mars), the refinement of nuclear fission as a power source and propulsive means will likely set the limits to optimal deep space propulsion for the foreseeable future. Costs, driven largely by access to space, continue to stall significant advances for both manned and unmanned missions. While there continues to be a hope that commercialization will lead to lower launch costs, the needed technology, initial capital investments, and markets have con- tinued to fail to materialize. Hence, initial development in deep space will likely remain govern- ment sponsored and driven by scientific goals linked to national prestige and perceived security issues. Against this backdrop, we consider linkage of scientific goals, current efforts, expecta- tions, current technical capabilities, and requirements for the detailed exploration of the solar system and consolidation of off-Earth outposts. Over the next century, distances of 50 AU could be reached by human crews but only if resources are brought to bear by international consortia. INTRODUCTION years hence, if that much3, usually – and rightly – that policy goals and technologies "Where there is no vision the people perish.” will change so radically on longer time scales – Proverbs, 29:181 that further extrapolation must be relegated to the realm of science fiction – or fantasy. -
Mars Exploration - a Story Fifty Years Long Giuseppe Pezzella and Antonio Viviani
Chapter Introductory Chapter: Mars Exploration - A Story Fifty Years Long Giuseppe Pezzella and Antonio Viviani 1. Introduction Mars has been a goal of exploration programs of the most important space agencies all over the world for decades. It is, in fact, the most investigated celestial body of the Solar System. Mars robotic exploration began in the 1960s of the twentieth century by means of several space probes sent by the United States (US) and the Soviet Union (USSR). In the recent past, also European, Japanese, and Indian spacecrafts reached Mars; while other countries, such as China and the United Arab Emirates, aim to send spacecraft toward the red planet in the next future. 1.1 Exploration aims The high number of mission explorations to Mars clearly points out the impor- tance of Mars within the Solar System. Thus, the question is: “Why this great interest in Mars exploration?” The interest in Mars is due to several practical, scientific, and strategic reasons. In the practical sense, Mars is the most accessible planet in the Solar System [1]. It is the second closest planet to Earth, besides Venus, averaging about 360 million kilometers apart between the furthest and closest points in its orbit. Earth and Mars feature great similarities. For instance, both planets rotate on an axis with quite the same rotation velocity and tilt angle. The length of a day on Earth is 24 h, while slightly longer on Mars at 24 h and 37 min. The tilt of Earth axis is 23.5 deg, and Mars tilts slightly more at 25.2 deg [2]. -
INTRODUCTION to SPACE EXPLORATION Creating a Time Capsule
INTRODUCTION TO SPACE EXPLORATION Creating a Time Capsule Grade Level: 5 - 8 Suggested TEKS Language Arts - 5.15 6.15 7.15 8.15 Social Studies - 5.18 6.20 7.20 8.20 Time Required: 30 - 45 minutes Art - 5.2 6.2 7.2 8.2 Computer - 5.2 6.2 7.2 8.2 Suggested SCANS Countdown: Writing paper Interpersonal. Interprets and Communicates Information National Science and Math Standards Pencils Science as Inquiry, Physical Science, Earth & Space Science, Science & Technology, History & Nature of Science, Measurement, Observing, Communicating Ignition: For decades, space colonies have been the creation of science fiction writers. However, with world population growing at an alarming rate, the concept of a second home in space could very likely become a stark reality. Already, a number of visionary scientists have drawn up plans for off-earth habitats. Biosphere II near Tucson, Arizona is an example. Additionally, NASA has future plans for a mission to Mars in the next 20 years. It certainly appears that earth will not always be our home. With this in mind, ask the students to consider the scenario suggested next in "Liftoff." Liftoff: You will have the opportunity to bury a time capsule, a sealed and durable box, which will be opened after one hundred years. Future discoverers of the box will be able to guess from the contents what your life was like 100 years before their time. Below are six different categories. For each category, choose an object that would best represent it. Keep in mind that you may choose items like photographs, scrapbooks, films or videos, books, newspapers, miniature models, and other favorite mementos. -
BAEN BOOKS TEACHER's GUIDE to GOING INTERSTELLAR Contents
BAEN BOOKS TEACHER’S GUIDE TO GOING INTERSTELLAR Contents: • recommended reading levels • plot summaries • essay outlines • character sketches • guides to each short story/essay including: o prepare to read… . vocabulary* . focus question/initiating activity o quiz/reading comprehension questions—multiple choice/short answer questions o critical thinking questions—higher order open-ended questions which might be utilized for quizzes/tests, class discussion, or essay prompts o suggested activities/inquiry-based exploration—suggestions for activities and projects Recommended reading levels: Going Interstellar is appropriate for a young adult audience. Classroom use of the book is most suitable for upper middle school to high school students. * Some texts in Going Interstellar contain an abundance of high-level vocabulary. For these texts, only the words and terms that are pertinent to supporting a scientific or thematic understanding are included in the “Prepare to Read” section. It is recommended that students use a dictionary while reading Going Interstellar. Background: Published by Baen books in 2012, this anthology combines short science fiction stories with scientific essays, each addressing theories and possible scenarios concerning interstellar space travel. Biographical information on the editors: • LES JOHNSON is a NASA physicist who is an expert on space propulsion systems. He is also a science fiction writer and the author of Back to the Moon. More information about Les can be found at his home website http://www.lesjohnsonauthor.com/. • JACK MCDEVITT has been publishing science fiction since 1981, and is the winner of multiple awards within the field. McDevitt’s devotion to scientifically accurate fiction is evident in his response to a question concerning how he prepares his novels: “The research is simple,” McDevitt says, “I pick up [a] phone and call a physicist” (www.sfwa.org). -
Aeronautics and Space Report of the President
Aeronautics and Space Report of the President 1971 Activities NOTE TO READERS: ALL PRINTED PAGES ARE INCLUDED, UNNUMBERED BLANK PAGES DURING SCANNING AND QUALITY CONTROL CHECK HAVE BEEN DELETED Aeronautics and Space Report of the President 197 I Activities i W Executive Office of the President National Aeronautics and Space Council Washington, D.C. 20502 PRESIDENT’S MESSAGE OF TRANSMITTAL To the Congress of the United States: I am pleased to transmit herewith a report of our national progress in aero- nautics and space activities during 1971. This report shows that we have made forward strides toward each of the six objectives which I set forth for a balanced space program in my statement of March 7, 1970. Aided by the improvements we have made in mobility, our explorers on the moon last summer produced new, exciting and useful evidence on the structure and origin of the moon. Several phenomena which they uncovered are now under study. Our unmanned nearby observation of Mars is similarly valuable and significant for the advancement of science. During 1971, we gave added emphasis to aeronautics activities which contribute substantially to improved travel conditions, safety and security, and we gained in- creasing recognition that space and aeronautical research serves in many ways to keep us in the forefront of man’s technological achievements. There can be little doubt that the investments we are now making in explora- tions of the unknown are but a prelude to the accomplishments of mankind in future generations. THEWHITE HOUSE, March 1972 iii Table of Contents Page Page I . Progress Toward U.S.