PEANUTS and SPACE FOUNDATION the Beagle Has Landed!
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
The Lost Indian Chandrayaan 2 Lander Vikram and Rover Pragyaan Found Intact in Single Piece on the Moon
ISSN (Online): 2350-0530 International Journal of Research -GRANTHAALAYAH ISSN (Print): 2394-3629 December 2020, Vol 8(12), 103 – 109 DOI: https://doi.org/10.29121/granthaalayah.v8.i12.2020.2608 THE LOST INDIAN CHANDRAYAAN 2 LANDER VIKRAM AND ROVER PRAGYAAN FOUND INTACT IN SINGLE PIECE ON THE MOON Jag Mohan Saxena 1 , H M Saxena *2 , Priyanka Saxena 3 1 Bldg. 1-E-19, Jai Narayan Vyas Nagar, Bikaner 334003, India *2 Geetanjali Aptts. 9FF, E Block, Rishi Nagar, Ludhiana 141001, India 3 Indian Institute of Technology, Jodhpur 342037, India DOI: https://doi.org/10.29121/granthaalayah.v8.i12.2020.2608 Article Type: Research Article ABSTRACT The Lunar Lander Vikram of the Moon Mission Chandrayaan 2 of the Article Citation: Jag Mohan Saxena, Indian Space Research Organization (ISRO) lost communication with the H M Saxena, and Priyanka Saxena. Lunar Orbiter and the mission control nearly 2.1 kms above the lunar (2020). THE LOST INDIAN surface during its landing on the Moon on 7th September, 2019. The exact CHANDRAYAAN 2 LANDER VIKRAM AND ROVER PRAGYAAN FOUND location and the sight of the lost lander and rover are still elusive. We INTACT IN SINGLE PIECE ON THE present here the exact location and first images of the lander Vikram and MOON. International Journal of rover Pragyaan sighted on the lunar surface. It is evident from the Research -GRANTHAALAYAH, processed images that the lander was intact and in single piece on landing 8(12), 103-109. away from the scheduled site and its ramp was deployed to successfully https://doi.org/10.29121/granthaa release the rover Pragyan on to the lunar surface. -
Orion First Flight Test
National Aeronautics and Space Administration orion First Flight Test NASAfacts Orion, NASA’s new spacecraft Exploration Flight Test-1 built to send humans farther During Orion’s flight test, the spacecraft will launch atop a Delta IV Heavy, a rocket built than ever before, is launching and operated by United Launch Alliance. While into space for the first time in this launch vehicle will allow Orion to reach an altitude high enough to meet the objectives for December 2014. this test, a much larger, human-rated rocket An uncrewed test flight called Exploration will be needed for the vast distances of future Flight Test-1 will test Orion systems critical to exploration missions. To meet that need, NASA crew safety, such as heat shield performance, is developing the Space Launch System, which separation events, avionics and software will give Orion the capability to carry astronauts performance, attitude control and guidance, farther into the solar system than ever before. parachute deployment and recovery operations. During the uncrewed flight, Orion will orbit The data gathered during the flight will influence the Earth twice, reaching an altitude of design decisions and validate existing computer approximately 3,600 miles – about 15 times models and innovative new approaches to space farther into space than the International Space systems development, as well as reduce overall Station orbits. Sending Orion to such a high mission risks and costs. altitude will allow the spacecraft to return to Earth at speeds near 20,000 mph. Returning -
Concept Study of a Cislunar Outpost Architecture and Associated Elements That Enable a Path to Mars
Concept Study of a Cislunar Outpost Architecture and Associated Elements that Enable a Path to Mars Presented by: Timothy Cichan Lockheed Martin Space [email protected] Mike Drever Lockheed Martin Space [email protected] Franco Fenoglio Thales Alenia Space Italy [email protected] Willian D. Pratt Lockheed Martin Space [email protected] Josh Hopkins Lockheed Martin Space [email protected] September 2016 © 2014 Lockheed Martin Corporation Abstract During the course of human space exploration, astronauts have travelled all the way to the Moon on short flights and have logged missions of a year or more of continuous time on board Mir and the International Space Station (ISS), close to Earth. However, if the long term goal of space exploration is to land humans on the surface of Mars, NASA needs precursor missions that combine operating for very long durations and great distances. This will allow astronauts to learn how to work in deep space for months at a time and address many of the risks associated with a Mars mission lasting over 1,000 days in deep space, such as the inability to abort home or resupply in an emergency. A facility placed in an orbit in the vicinity of the Moon, called a Deep Space Transit Habitat (DSTH), is an ideal place to gain experience operating in deep space. This next generation of in-space habitation will be evolvable, flexible, and modular. It will allow astronauts to demonstrate they can operate for months at a time beyond Low Earth Orbit (LEO). The DSTH can also be an international collaboration, with partnering nations contributing elements and major subsystems, based on their expertise. -
Lunar Programs
LUNAR PROGRAMS NASA is leading a sustainable return to the Moon Aerospace is partnered with NASA to with commercial and international partners to return humans to the Moon in every expand human presence in space and gather phase and journey, including the: new knowledge and opportunities. In 2017, Space › Planning and supporting the Policy Directive-1 called for a renewed emphasis on first lifecycle review of the commercial and international partnerships, return Gateway Initiative of humans to the Moon for long-term exploration and utilization followed by human missions to Mars. › Design, systems engineering and Aerospace is partnered with NASA in this endeavor integration, and operational concepts and is involved in every phase and journey. of the EVA system Artist’s conception of a gateway habitat. Image credit: NASA Humans must return to the moon for long-term › Ground testing of the NEXTStep deep exploration and utilization of deep space, but lunar space habitat module prototypes exploration is more than a stepping stone to Mars missions. The phased plan includes › Design and test of the Orion sending missions to the moon and cislunar space for exploration and study, and the capsule avionics construction of the Deep Space Gateway, a space station intended to orbit the moon. Aerospace provides support to these missions in areas such as systems engineering and integration, program management, and various subsystem expertise. Current Lunar Programs GATEWAY INITIATIVE NASA’s Gateway is conceived to be an exploration and science outpost in orbit around the moon that will enable human crewed missions to both cislunar space and the moon’s surface, meet scientific discovery and exploration objectives, and demonstrate and prove enabling technologies through commercial and international partnerships. -
Conceptual Human-System Interface Design for a Lunar Access Vehicle
Conceptual Human-System Interface Design for a Lunar Access Vehicle Mary Cummings Enlie Wang Cristin Smith Jessica Marquez Mark Duppen Stephane Essama Massachusetts Institute of Technology* Prepared For Draper Labs Award #: SC001-018 PI: Dava Newman HAL2005-04 September, 2005 http://halab.mit.edu e-mail: [email protected] *MIT Department of Aeronautics and Astronautics, Cambridge, MA 02139 TABLE OF CONTENTS 1 INTRODUCTION..................................................................................................... 1 1.1 THE GENERAL FRAMEWORK................................................................................ 1 1.2 ORGANIZATION.................................................................................................... 2 2 H-SI BACKGROUND AND MOTIVATION ........................................................ 3 2.1 APOLLO VS. LAV H-SI........................................................................................ 3 2.2 APOLLO VS. LUNAR ACCESS REQUIREMENTS ...................................................... 4 3 THE LAV CONCEPTUAL PROTOTYPE............................................................ 5 3.1 HS-I DESIGN ASSUMPTIONS ................................................................................ 5 3.2 THE CONCEPTUAL PROTOTYPE ............................................................................ 6 3.3 LANDING ZONE (LZ) DISPLAY............................................................................. 8 3.3.1 LZ Display Introduction................................................................................. -
Orion Capsule Launch Abort System Analysis
Orion Capsule Launch Abort System Analysis Assignment 2 AE 4802 Spring 2016 – Digital Design and Manufacturing Georgia Institute of Technology Authors: Tyler Scogin Michel Lacerda Jordan Marshall Table of Contents 1. Introduction ......................................................................................................................................... 4 1.1 Mission Profile ............................................................................................................................. 7 1.2 Literature Review ........................................................................................................................ 8 2. Conceptual Design ............................................................................................................................. 13 2.1 Design Process ........................................................................................................................... 13 2.2 Vehicle Performance Characteristics ......................................................................................... 15 2.3 Vehicle/Sub-Component Sizing ................................................................................................. 15 3. Vehicle 3D Model in CATIA ................................................................................................................ 22 3.1 3D Modeling Roles and Responsibilities: .................................................................................. 22 3.2 Design Parameters and Relations:............................................................................................ -
Gao-21-330, Nasa Lunar Programs
Report to Congressional Committees May 2021 NASA LUNAR PROGRAMS Significant Work Remains, Underscoring Challenges to Achieving Moon Landing in 2024 GAO-21-330 May 2021 NASA LUNAR PROGRAMS Significant Work Remains, Underscoring Challenges to Achieving Moon Landing in 2024 Highlights of GAO-21-330, a report to congressional committees Why GAO Did This Study What GAO Found In March 2019, the White House The National Aeronautics and Space Administration (NASA) has initiated eight directed NASA to accelerate its plans lunar programs since 2017 to help NASA achieve its goal of returning humans to for a lunar landing by 4 years, to 2024. the Moon. NASA plans to conduct this mission, known as Artemis III, in 2024. Accomplishing this goal will require NASA has made progress by completing some early lunar program development extensive coordination across lunar activities including initial contract awards, but an ambitious schedule decreases programs and contractors to ensure the likelihood of NASA achieving its goal. For example, NASA’s planned pace to systems operate together seamlessly develop a Human Landing System, shown below, is months faster than other and safely. In December 2019, GAO spaceflight programs, and a lander is inherently more complex because it found that NASA had begun making supports human spaceflight. decisions related to requirements, cost, and schedule for individual lunar Notional Human Landing System programs but was behind in taking these steps for the Artemis III mission. The House Committee on Appropriations included a provision in 2018 for GAO to review NASA’s proposed lunar-focused programs. This is the second such report. -
Space Sector Brochure
SPACE SPACE REVOLUTIONIZING THE WAY TO SPACE SPACECRAFT TECHNOLOGIES PROPULSION Moog provides components and subsystems for cold gas, chemical, and electric Moog is a proven leader in components, subsystems, and systems propulsion and designs, develops, and manufactures complete chemical propulsion for spacecraft of all sizes, from smallsats to GEO spacecraft. systems, including tanks, to accelerate the spacecraft for orbit-insertion, station Moog has been successfully providing spacecraft controls, in- keeping, or attitude control. Moog makes thrusters from <1N to 500N to support the space propulsion, and major subsystems for science, military, propulsion requirements for small to large spacecraft. and commercial operations for more than 60 years. AVIONICS Moog is a proven provider of high performance and reliable space-rated avionics hardware and software for command and data handling, power distribution, payload processing, memory, GPS receivers, motor controllers, and onboard computing. POWER SYSTEMS Moog leverages its proven spacecraft avionics and high-power control systems to supply hardware for telemetry, as well as solar array and battery power management and switching. Applications include bus line power to valves, motors, torque rods, and other end effectors. Moog has developed products for Power Management and Distribution (PMAD) Systems, such as high power DC converters, switching, and power stabilization. MECHANISMS Moog has produced spacecraft motion control products for more than 50 years, dating back to the historic Apollo and Pioneer programs. Today, we offer rotary, linear, and specialized mechanisms for spacecraft motion control needs. Moog is a world-class manufacturer of solar array drives, propulsion positioning gimbals, electric propulsion gimbals, antenna positioner mechanisms, docking and release mechanisms, and specialty payload positioners. -
Concept for a Crewed Lunar Lander Operating from the Lunar Orbiting Platform-Gateway
69th International Astronautical Congress (IAC), Bremen, Germany, 1-5 October 2018. Copyright © 2018 by Lockheed Martin Corporation. Published by the IAF, with permission and released to the IAF to publish in all forms. IAC-18.A5.1.4x46653 Concept for a Crewed Lunar Lander Operating from the Lunar Orbiting Platform-Gateway Timothy Cichana*, Stephen A. Baileyb, Adam Burchc, Nickolas W. Kirbyd aSpace Exploration Architect, P.O. Box 179, MS H3005, Lockheed Martin Space, Denver, Colorado, U.S.A. 80201, [email protected] bPresident, 8100 Shaffer Parkway, Unit 130, Deep Space Systems, Inc., Littleton, Colorado, 80127-4124, [email protected] cDesign Engineer / Graphic Artist, 8341 Sangre de Christo Rd, Deep Space Systems, Inc., Littleton, Colorado, 80127, [email protected] dSystems Engineer, Advanced Programs, P.O. Box 179, MS H3005, Lockheed Martin Space, Denver, Colorado, U.S.A. 80201, [email protected] * Corresponding Author Abstract Lockheed Martin is working with NASA on the development of the Lunar Orbiting Platform – Gateway, or Gateway. Positioned in the vicinity of the Moon, the Gateway allows astronauts to demonstrate operations beyond Low Earth Orbit for months at a time. The Gateway is evolvable, flexible, modular, and is a precursor and mission demonstrator directly on the path to Mars. Mars Base Camp is Lockheed Martin's vision for sending humans to Mars. Operations from an orbital base camp will build on a strong foundation of today's technologies and emphasize scientific exploration as mission cornerstones. Key aspects of Mars Base Camp include utilizing liquid oxygen and hydrogen as the basis for a nascent water-based economy and the development of a reusable lander/ascent vehicle. -
Lunar Lander Educator Edition
National Aeronautics and Space Administration Geometry and Algebra II Grade Level THE LUNAR LANDER – Ascending from the Moon 9-12 Instructional Objectives Subject Area Mathematics: Geometry Students will and Algebra II • use trigonometric function rules to solve problems • graph and analyze functions to determine a relationship between Key Concept two variables Application of trigonometric functions Prerequisites Teacher Prep Time Students should have a good knowledge of right triangle trigonometry and 15 minutes how to solve problems using trigonometric functions and inverse trigonometric functions. Students should also be able to manipulate and Problem Duration evaluate functions. 45-60 minutes Background Technology Graphing Calculator This problem is part of a series of problems that apply Algebra and Geometry principles to U.S. Space Exploration policy. Materials Exploration provides the foundation of our knowledge, technology, Student Edition resources, and inspiration. It seeks answers to fundamental questions about our existence, responds to recent discoveries and puts in place Degree of Difficulty revolutionary techniques and capabilities to inspire our nation, the world, Moderate to Difficult and the next generation. Through NASA, we touch the unknown, we learn and we understand. As we take our first steps toward sustaining a human Skill presence in the solar system, we can look forward to far-off visions of the Operations with past becoming realities of the future. trigonometric functions; manipulating and The vision for space exploration includes returning the space shuttle evaluating functions; safely to flight, completing the International Space Station, developing a graphing; calculator use new exploration vehicle and all the systems needed for embarking on extended missions to the Moon, Mars, and beyond. -
Designing a Lunar Lander
Designing a Lunar Lander Supplies You’ll Need: Any clean, recyclable items that you find around your house, for example: paper towel or bathroom rolls, paper plates and utensils, plastic cups, bottles, caps, etc...aluminum foil, paper and/or plastic bags, party supplies – like hats, balloons, streamers, wrapping paper; paper clips, envelopes, old stuff from your garage like string, rope, twist ties, wire, strong tape, glue – anything works – get creative!! Before You Begin: Think about your design, it helps if you make a plan, or drawing. Here are some things to think about. The NASA Artemis Mission – Return to the Moon by 2024! Imagine that you are part of the new Artemis Mission team, designing a Lunar Lander that will help astronauts return to the moon by the year 2024. Your Lander must: • Disconnect, and reconnect later, with the Command Module • Have a way of moving through space on its own • Have space for the crew to live (sleep, eat, work, and pilot the lander) while they are on the moon • Land safely on the moon and lift off again • Have at least 1 hatch where astronauts can get in and out after landing on the moon • Have a way for astronauts to safely get in and out of the lander while it’s connected the Command Module in space Take a few minutes to think about what your Lander will need. Imagine what it will look like. Draw the exterior (outside) of your Lander below, and label the important parts! Use this drawing to guide you as you build. -
The New Vision for Space Exploration
Constellation The New Vision for Space Exploration Dale Thomas NASA Constellation Program October 2008 The Constellation Program was born from the Constellation’sNASA Authorization Beginnings Act of 2005 which stated…. The Administrator shall establish a program to develop a sustained human presence on the moon, including a robust precursor program to promote exploration, science, commerce and U.S. preeminence in space, and as a stepping stone to future exploration of Mars and other destinations. CONSTELLATION PROJECTS Initial Capability Lunar Capability Orion Altair Ares I Ares V Mission Operations EVA Ground Operations Lunar Surface EVA EXPLORATION ROADMAP 0506 07 08 09 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 LunarLunar OutpostOutpost BuildupBuildup ExplorationExploration andand ScienceScience LunarLunar RoboticsRobotics MissionsMissions CommercialCommercial OrbitalOrbital Transportation ServicesServices forfor ISSISS AresAres II andand OrionOrion DevelopmentDevelopment AltairAltair Lunar LanderLander Development AresAres VV and EarthEarth DepartureDeparture Stage SurfaceSurface SystemsSystems DevelopmentDevelopment ORION: NEXT GENERATION PILOTED SPACECRAFT Human access to Low Earth Orbit … … to the Moon and Mars ORION PROJECT: CREW EXPLORATION VEHICLE Orion will support both space station and moon missions Launch Abort System Orion will support both space stationDesigned and moonto operate missions for up to 210 days in Earth or lunar Designedorbit to operate for up to 210 days in Earth or lunar orbit Designed for lunar