AstroMast Continuous Longeron Mast History
|
|
- Baldric Logan
- 6 years ago
- Views:
Transcription
1 AstroMast Programs
2 AstroMasts Astro has flown deployable AstroMasts on many Major Space Programs These have included major NASA and DOD programs such as GOES, DMSP and Milstar All flights have been successful DMSP still has remaining masts on the ground ready for flight AstroMast Continuous Longeron Mast History Program Masts Delivered Masts Flown Purpose Flew Customer Type Length S Magnetometer 1974 Air Force Lanyard 6-meters Voyager 3 3 Magnetometer 1977 JPL Lanyard 13-meters Nova 1 1 Gravity Gradient 1981 RCA Lanyard 25 ft Solar Max 1 1 Antenna 1980 Sperry Lanyard 6 ft Dynamic Explorer 3 3 instruments + Magnetometer 1981 RCA Lanyard 20 ft INSAT 4 4 Solar Sail Ford Lanyard 43ft Olympus 2 2 Solar Array 1984 Fokker Canister 28ft CRRES 1 1 Spectrometer 1990 Ball Lanyard 9-meters Milstar Milstar LMSC Canister 30 ft Mars Observer 2 2 Magnetometer 1992 GE/LMCS Canister 6-meters GOES 5 5 Solar Sail Loral Lanyard 53 ft MTSAT 2 2 Solar Sail 2006 Loral Lanyard 65-ft DMSP 5 2 Magnetometer Lockheed Lanyard 6-meters MRO 1 1 Gamma Ray Spectrometer 2005 Lockheed Lanyard 6-meters
3 Solar Sail MTSAT/GOES/INSAT 9-Inch AstroMast Lanyard Deployed 17-Meter Length (GOES) 13-Meter Length (INSAT) Motor Controlled 10-Foot Solar Torquer Sail Aluminized Kapton Customer: Space Systems/Loral
4 Antenna Systems FORTÉ AstroMast deploys quadrapole antenna along spacecraft yaw axis Titanium Antenna element Canister mounts to deck of spacecraft 10-inch mast: self deploying, straight (no pretwist), root deploying with torsion spring assist at root Controlled by eddy current damper and lanyard Weight kg (34.76 lb) Customer: Los Alamos National Laboratory
5 Instrument Boom DMSP Magnetometer 10-Inch AstroMast Lanyard Deployed 6-Meter Length Eddy Current Damper Controlled Supports Magnetometer Instrument Customer: Lockheed Martin
6 Solar Array Actuator MILSTAR AstroMast 10-inch-diameter AstroMast Canister deployed 16-meter length Brushless motor controlled Solar array deployer Customer: Lockheed Martin
7 Astromasts Unidirectional high strain glass-epoxy members High strength/weight 0.07% packing factor Non-Magnetic Mast can self deploy as in the DMSP Magnetometer Boom Mast can be nut-driven as in the Milstar Solar Array deployer to provide high deployment force Milstar DMSP Principles Longerons coil down for stowage The Battens are relaxed when stowed The longerons self straighten when deploying, tensioning diagonals which bow the battens and preload the resulting truss structure
8 MTSAT/GOES/INSAT 9-Inch AstroMast Lanyard Deployed 17-Meter Length (GOES) 13-Meter Length (INSAT) Motor Controlled 10-Foot Solar Torquer Sail Aluminized Kapton Customer: Space Systems/Loral
9 MARS Observer GRS Boom 10-Inch AstroMast Canister Deployed Deployed 6-Meter Length Brushless DC Motor Deployed Supports Gamma Ray Spectrometer Customer: Space Systems/Loral
10 DMSP Magnetometer Boom 10-Inch AstroMast Lanyard Deployed 6-Meter Length Eddy Current Damper Controlled Supports Magnetometer Instrument Customer: Lockheed Martin
11 FORTÉ Antenna System Feature Astromast deploys quadrapole antenna along spacecraft yaw axis s Ten canisters stow antenna element in wrapped helix Antenna element is titanium wire Canister mounts to deck of spacecraft Simple eight-hole interface to spacecraft, six holes on tip plate 10-inch mast: self deploying, straight (no pretwist), root deploying with torsion spring assist at root Tie-rod launch restraint HOP actuator initiation Deployment controlled by eddy current damper and lanyard Weight budget: kg (34.76 lb)
12 MILSTAR AstroMast 10-inch-diameter AstroMast Canister deployed 16-meter length Brushless motor controlled Solar array deployer Customer: Lockheed Martin Astro Aerospace
13
Technical Verification Satellite STARS for Tethered Space Robot
Technical Verification Satellite STARS for Tethered Space Robot Masahiro Nohmi, Takeshi Yamamoto, and Akira Andatsu Kagawa University nohmi@eng.kagawa-u.ac.jp, s05g528@stmail.eng.kagawa-u.ac.jp, s06g452@stmail.eng.kagawa-u.ac.jp
More informationLecture Module 5: Introduction to Attitude Stabilization and Control
1 Lecture Module 5: Introduction to Attitude Stabilization and Control Lectures 1-3 Stability is referred to as a system s behaviour to external/internal disturbances (small) in/from equilibrium states.
More informationPaper Session III-B - Mars Global Surveyor: Cruising to Mars
The Space Congress Proceedings 1997 (34th) Our Space Future - Uniting For Success May 1st, 1:00 PM Paper Session III-B - Mars Global Surveyor: Cruising to Mars Glenn E. Cunningham Project Manager Mars
More informationBall Aerospace & Technologies Corp. & L Garde Inc.
Ball Aerospace & Technologies Corp. & L Garde Inc. Rapid De-Orbit of LEO Space Vehicles Using Towed owed Rigidizable Inflatable nflatable Structure tructure (TRIS) Technology: Concept and Feasibility Assessment
More informationStarshade Technology Status
Jet Propulsion Laboratory California Institute of Technology Starshade Technology Status Stuart Shaklan and Nick Siegler NASA Exoplanet Exploration Program November 3, 2016 California Institute of Technology.
More informationPointing Control for Low Altitude Triple Cubesat Space Darts
Pointing Control for Low Altitude Triple Cubesat Space Darts August 12 th, 2009 U.S. Naval Research Laboratory Washington, D.C. Code 8231-Attitude Control System James Armstrong, Craig Casey, Glenn Creamer,
More informationAdvanced Probes for Planetary Surface and Subsurface Exploration
Workshop on Space Robotics, ICRA 2011 Advanced Probes for Planetary Surface and Subsurface Exploration Takashi Kubota (JAXA/ISAS/JSPEC) Hayato Omori, Taro Nakamura (Chuo Univ.) JAXA Space Exploration Program
More informationChallenges in Realizing Large Structures in Space
Challenges in Realizing Large Structures in Space Gunnar Tibert KTH Space Center Space Rendezvous, 13 Oct 2016 Large Structures in Space My experience on large space structures: Centrifugally deployed
More informationRF APERTURE ARCHITECTURES 11 Nov. 08
RF APERTURE ARCHITECTURES 11 Nov. 08 r. Thomas Murphey Space Vehicles irectorate Mitigating Structural eformations Mitigating structural deformations in large apertures: There is always a trade between
More informationLaunches and On-Orbit Performance
Launches and On-Orbit Performance An Update on Nanosatellite Missions at the UTIAS Space Flight Laboratory Daniel D. Kekez,, Robert E. Zee, Freddy M. Pranajaya Space Flight Laboratory University of Toronto
More informationExploration Carriers UPC-Orion Launch Opportunities for Lunar Missions. presented to The Joint Annual Meeting of LEAG-ICEUM-SRR
Exploration Carriers UPC-Orion Launch Opportunities for Lunar Missions presented to The Joint Annual Meeting of LEAG-ICEUM-SRR Bruce Milam and Ruthan Lewis, Ph.D. NASA Goddard Space Flight Center October
More informationEnabling Low Cost Planetary Missions Through Rideshare Opportuni;es
Enabling Low Cost Planetary Missions Through Rideshare Opportuni;es J. J. Lang, J. D. Baker, T. P. McElrath, T. Moreno, J. S. Snyder / California InsCtute of Technology June 20, 2013 A Low Cost Approach
More informationFORMOSAT-3 Satellite Thermal Control Design and Analysis *
Journal of Aeronautics, Astronautics and Aviation, Series A, Vol.39, No.4, pp.287-292 (27) 287 Technical Note FORMOSAT-3 Satellite Thermal Control Design and Analysis * Ming-Shong Chang **, Chia-Ray Chen,
More informationMars Sample Return (MSR) Mission BY: ABHISHEK KUMAR SINHA
Mars Sample Return (MSR) Mission BY: ABHISHEK KUMAR SINHA Samples returned to terrestrial laboratories by MSR Mission would be analyzed with state-of the-art instrumentation providing unprecedented insight
More informationSmall Satellite Platform Imaging X-Ray Polarimetry Explorer (IXPE) Mission Concept and Implementation
Small Satellite Platform Imaging X-Ray Polarimetry Explorer (IXPE) Mission Concept and Implementation 31 st Annual AIAA/USU Conference on Small Satellites Utah State University, Logan, UT, USA August 6-10,
More informationBoom-Membrane Integrated Deployable Structures for De-orbiting Satellites and Future Applications
Boom-Membrane Integrated Deployable Structures for De-orbiting Satellites and Future Applications Hiroshi Furuya furuya@enveng.titech.ac.jp Tokyo Institute of Technology, ORIGAMI Project (ORganizatIon
More informationAIR BEARING ADCS TEST BED. Daniel E. Wukelic College of Engineering University of Hawai i at Mānoa Honolulu, HI ABSTRACT INTRODUCTION
AIR BEARING ADCS TEST BED Daniel E. Wukelic College of Engineering University of Hawai i at Mānoa Honolulu, HI 96822 ABSTRACT The Hawai i Space Flight Laboratory (HSFL) designs, tests and builds small
More informationENGN1300: Structural Analysis. Spring, 2010
Division of Engineering Brown University ENGN1300: Structural Analysis Spring, 2010 The goal of the course is to enable you to analyze relatively complex structures by creating appropriate mathematical
More informationINCA. Ionospheric Neutron Content Analyzer. New Mexico State University University NanoSat-8. CubeSat Workshop Presentation August 2, 2014; Logan, UT
INCA Ionospheric Neutron Content Analyzer New Mexico State University University NanoSat-8 CubeSat Workshop Presentation August 2, 2014; Logan, UT Presentation Outline Mission Overview Mission Relevance
More informationINCA. Ionospheric Neutron Content Analyzer. New Mexico State University University NanoSat-8. CubeSat Workshop Presentation August 2, 2014; Logan, UT
INCA Ionospheric Neutron Content Analyzer New Mexico State University University NanoSat-8 CubeSat Workshop Presentation August 2, 2014; Logan, UT Mission Overview Mission Relevance ConOps INCA Payload
More informationShape Accuracy of a Joint-Dominated Deployable Mast
Shape Accuracy of a Joint-Dominated Deployable Mast O.R. Stohlman and S. Pellegrino California Institute of Technology, Pasadena, CA 91125 This paper presents a study to capture and model friction related
More informationStructural Scaling Metrics For Tensioned-Blanket Space Systems
University of New Mexico UNM Digital Repository Civil Engineering ETDs Engineering ETDs 7-12-2014 Structural Scaling Metrics For Tensioned-Blanket Space Systems Jeremy Banik Follow this and additional
More informationSOLAR BLADE NANOSATELLITE DEVELOPMENT: HELIOGYRO DEPLOYMENT, DYNAMICS, AND CONTROL
SOLAR BLADE NANOSATELLITE DEVELOPMENT: HELIOGYRO DEPLOYMENT, DYNAMICS, AND CONTROL Carnegie Mellon University, 5000 Forbes Ave., Pittsburgh, PA 15213 rsb@frc.ri.cmu.edu Abstract Nanosats are a new class
More informationSTS41-D Solar Array Flight Experiment
The Space Congress Proceedings 1984 (21st) New Opportunities In Space Apr 1st, 8:00 AM STS41-D Solar Array Flight Experiment Gary F. Turner Manager, Solar Array Programs Lockheed Missiles & Space Co.,
More informationSOLAR BLADE NANOSATELLITE DEVELOPMENT. Richard Blomquist Carnegie Mellon University 5000 Forbes Ave., Pittsburgh, PA
SOLAR BLADE NANOSATELLITE DEVELOPMENT. Richard Blomquist Carnegie Mellon University 5000 Forbes Ave., Pittsburgh, PA 15213 rsb@frc.ri.cmu.edu Abstract Nanosats are a new class of low mass satellite amenable
More informationE D D Y C U R R E N T D A M P E R A P P L I C AT I O N D ATA
E D D Y C U R R E N T D A M P E R A P P I C AT I O N D ATA CDA InterCorp CDA InterCorp INTRODUCTION This application manual defines the performance capabilities of CDA InterCorp s Eddy Current Damper Product
More informationI I I I I I I I I I I I I I THE SPACE TEST PROGRAM APEX MISSION SATELLITE. Frank L. Knight The Aerospace Corporation Los Angeles, CA
Abstract An overview is presented of the Air Force Space Test Program's Advanced Photovoltaic And Electronic Experiments (APEX) Mission. APEX will provide spaceflight for three military experiments on
More information5.6 Work. Common Units Force Distance Work newton (N) meter (m) joule (J) pound (lb) foot (ft) Conversion Factors
5.6 Work Page 1 of 7 Definition of Work (Constant Force) If a constant force of magnitude is applied in the direction of motion of an object, and if that object moves a distance, then we define the work
More informationRepeatability of joint-dominated deployable masts
Repeatability of joint-dominated deployable masts Thesis by Olive R Stohlman In Partial Fulfillment of the Requirements for the Degree of Doctor of Philosophy California Institute of Technology Pasadena,
More informationGOES-R Instrument Status and Accommodations. Barbara Pfarr GOES-R Program Systems Engineering January 2010 AMS Conference
GOES-R Instrument Status and Accommodations Barbara Pfarr GOES-R Program Systems Engineering January 2010 AMS Conference Agenda Instrument Developmental Status Significant Changes in the Last Year Introducing
More informationAttitude Control on the Pico Satellite Solar Cell Testbed-2
SSC12-II-1 Attitude Control on the Pico Satellite Solar Cell Testbed-2 Siegfried W. Janson, Brian S. Hardy, Andrew Y. Chin, Daniel L. Rumsey, Daniel A. Ehrlich, and David A. Hinkley The Aerospace Corporation
More informationThe E-SAIL programme. 10th IAA Symposium on Small Satellites for Earth Observation April 20-24, 2015 Berlin LuxSpace s.à.r.
The E-SAIL programme 10th IAA Symposium on Small Satellites for Earth Observation April 20-24, 2015 Berlin LuxSpace s.à.r.l An OHB company Contents LuxSpace Background Consortium Spacecraft Specific issues
More informationMicro Gravity Balloon Drop: Tether Release
A B d ε g h I L m Ω P r Micro Gravity Balloon Drop: Tether Release Natalie A. Ramm 1 and Bill G. Solyst 2 Taylor University, Upland, IN, 46989 Ben C. Fisher 3 and Reid E. Dodge 4 Taylor University, Upland,
More informationAr in Mars Atmosphere: A Good Tracer for Meridional Mixing. GRS Team
Ar in Mars Atmosphere: A Good Tracer for Meridional Mixing GRS Team Ann L. Sprague, William V. Boynton, Kris E. Kerry, Daniel M. Janes, Donald M. Hunten Lunar and Planetary Laboratory University of Arizona
More informationInflatable Space Structures
Inflatable Space Structures Matthew Allgeier Erin Kelly ASEN 5519 Final Presentation Inflatable Space Structures 1 Presentation Overview Introduction Background Technical issues Applications Environmental
More informationSCIENCE WITH DIRECTED AERIAL DR. ALEXEY PANKINE GLOBAL AEROSPACE CORPORATION SAILING THE PLANETS
: SCIENCE WITH DIRECTED AERIAL ROBOT EXPLORERS (DARE) DR. ALEXEY PANKINE GLOBAL AEROSPACE CORPORATION 1 NEW ARCHITECTURE FOR PLANETARY EXPLORATION KEY ELEMENTS: Long-Duration Planetary Balloon Platforms
More informationDevelopment of Deployment System for Small Size Solar Sail Mission
Trans. JSASS Space Tech. Japan Vol. 7, No. ists6, pp. Pd_87-Pd_9, 9 Development of Deployment System for Small Size Solar Sail Mission By Osamu MORI, ) Hirotaka SAWADA, ) Fuminori HANAOKA, ) Junichiro
More informationMSL PYROSHOCK DEVELOPMENT TEST PROGRAM FOR SHOCK MITIGATION. Juan Pablo Fernández
ICSV14 Cairns Australia 9-12 July, 2007 MSL PYROSHOCK DEVELOPMENT TEST PROGRAM FOR SHOCK MITIGATION Abstract Juan Pablo Fernández Jet Propulsion Laboratory, California Institute of Technology 4800 Oak
More informationNASA JPL/NSTA Web Seminar: Robotic Exploration of the Red Planet
LIVE INTERACTIVE LEARNING @ YOUR DESKTOP NASA JPL/NSTA Web Seminar: Robotic Exploration of the Red Planet Wednesday, May 14, 2008 Robotic Exploration of the Red Planet Greg Mehall Arizona State University
More informationSatellite Components & Systems. Dr. Ugur GUVEN Aerospace Engineer (P.hD) Nuclear Science & Technology Engineer (M.Sc)
Satellite Components & Systems Dr. Ugur GUVEN Aerospace Engineer (P.hD) Nuclear Science & Technology Engineer (M.Sc) Definitions Attitude: The way the satellite is inclined toward Earth at a certain inclination
More informationInterstellar Exploration Through Repeated External Acceleration
Interstellar Exploration Through Repeated External Acceleration Andrew Bingham NIAC Student Fellows Prize Department of Mechanical and Aeronautical Engineering, Clarkson University NIAC Fellows Meeting,
More informationMake Your Cubesat Overnight and Put it in Any Orbit (Well almost)
Make Your Cubesat Overnight and Put it in Any Orbit (Well almost) Jim White, Walter Holemans, Planetary Systems Inc. Dr. Adam Huang, University of Arkansas RAMPART Summary Main Components The Promise of
More informationWhat s Up in Space? Dean W McCall, Ed.D.
What s Up in Space? Dean W McCall, Ed.D. In no particular order Brief aerospace CV Systems Engineering Space mission types Examples Gotchas Terminology & Slang Please ask questions McCall Background Hughes
More informationSix Days at the Edge of Space: 10 Years of HASP Balloon Flight Operations
Six Days at the Edge of Space: 10 Years of HASP Balloon Flight Operations T. Gregory Guzik, Louisiana Space Grant Consortium Department of Physics & Astronomy Louisiana State University v030316 1 Primary
More informationCompact, lightweight, and athermalized mirror and mount for use on JWST's NIRCam instrument
Compact, lightweight, and athermalized mirror and mount for use on JWST's NIRCam instrument Derek Edinger, Paul Mammini*, Liz Osborne Lockheed Martin Advanced Technology Center, 3251 Hanover St., Palo
More informationABSTRACT. IAI-MLM designs and manufactures solar panels. The present analysis was conducted within one of the current projects.
ANALYSIS OF A SATELLITE SOLAR ARRAY DEPLOYMENT BY MSC.ADAMS Paper No. 2004-37 By Zvi Zaphir and Moshe Halfon, Israel aircraft Industries, MLM division, Israel* ABSTRACT IAI-MLM designs and manufactures
More informationCommunication. Provides the interface between ground and the spacecraft Functions:
Telecomm Communication Provides the interface between ground and the spacecraft Functions: Lock onto the ground station signal (carrier tracking) Receive uplink and process it (command reception and detection)
More informationCreating Large Space Platforms From Small Satellites
SSC99-VI-6 Creating Large Space Platforms From Small Satellites Andrew W. Lewin Principal Systems Engineer Orbital Sciences Corporation Dulles, VA 20166 (703) 406-5000 lewin.andy@orbital.com Abstract.
More informationINTERNATIONAL SPACE STATION, A DEPLOYMENT AND MODAL TEST FACILITY
IAC-02-1.2.06 INTERNATIONAL SPACE STATION, A DEPLOYMENT AND MODAL TEST FACILITY Sherry Draisey President, Good Vibrations Engineering Ltd. Toronto, Canada sherry@gve.on.ca ABSTRACT The International Space
More informationApplications of Integration to Physics and Engineering
Applications of Integration to Physics and Engineering MATH 211, Calculus II J Robert Buchanan Department of Mathematics Spring 2018 Mass and Weight mass: quantity of matter (units: kg or g (metric) or
More informationFlight Demonstration of Electrostatic Thruster Under Micro-Gravity
Flight Demonstration of Electrostatic Thruster Under Micro-Gravity Shin SATORI*, Hiroyuki MAE**, Hiroyuki OKAMOTO**, Ted Mitsuteru SUGIKI**, Yoshinori AOKI # and Atsushi NAGATA # * Hokkaido Institute of
More informationPerformance Validation of the Triangular Rollable and Collapsible Mast
Performance Validation of the Triangular Rollable and Collapsible Mast Jeremy A. Banik & Thomas W. Murphey Air Force Research Laboratory, Space Vehicles Directorate, Kirtland AFB, NM 87117 Afrl.rvsv@kirtland.af.mil
More informationLearning Lab Seeing the World through Satellites Eyes
Learning Lab Seeing the World through Satellites Eyes ESSENTIAL QUESTION What is a satellite? Lesson Overview: Engage students will share their prior knowledge about satellites and explore what satellites
More informationAS3010: Introduction to Space Technology
AS3010: Introduction to Space Technology L E C T U R E 22 Part B, Lecture 22 19 April, 2017 C O N T E N T S Attitude stabilization passive and active. Actuators for three axis or active stabilization.
More informationEng Sample Test 4
1. An adjustable tow bar connecting the tractor unit H with the landing gear J of a large aircraft is shown in the figure. Adjusting the height of the hook F at the end of the tow bar is accomplished by
More informationSmall Satellite Deployments From STS116 - Development Of New Manned Spaceflight Deployment Systems
SSC07-III-1 Small Satellite Deployments From STS116 - Development Of New Manned Spaceflight Deployment Systems Perry G. Ballard, Albert Meza DOD Space Test Program Scott Ritterhouse, Theresa Shaffer, Carolynn
More informationRobotic Assembly of a 20-Meter Space Telescope With Extension to 40-Meter Telescopes
Robotic Assembly of a 20-Meter Space Telescope With Extension to 40-Meter Telescopes Presented at the Ultra Lightweight Space Optics Workshop March 25, 1999 By Ronald M. Muller The Boeing Company Engineering
More informationAttitude Determination and. Attitude Control
Attitude Determination and Placing the telescope in orbit is not the end of the story. It is necessary to point the telescope towards the selected targets, or to scan the selected sky area with the telescope.
More informationNew Worlds Observer Final Report Appendix E. Section E: Starshades Subsection E.6: Starshade Spacecraft Lead Author: Amy Lo
Section E: Starshades Subsection E.6: Starshade Spacecraft Lead Author: Amy Lo Introduction Starshade Spacecraft Functional Requirements The main function of the starshade spacecraft is to: 1) support
More informationSECTION 1 - WHAT IS A BTU METER? BTU's = Flow x ΔT Any ISTEC BTU Meter System consists of the following main components:
SECTION 1 - WHAT IS A BTU METER? ISTEC BTU Meters measure energy usage by multiplying flow rate and temperature difference. As the water (or other liquid) passes through these lines, the multi-wing turbine
More informationOpportunities for Small Satellites and Space Research Using the K-1 Vehicle
SSC99-X-5 Opportunities for Small Satellites and Space Research Using the K-1 Vehicle Debra Facktor Lepore, Gary Lai, and Tom Taylor Kistler Aerospace Corporation 3760 Carillon Point, Kirkland, Washington
More informationDEVELOPMENT OF INNOVATIVE MECHANICAL FLEXIBLE SOLAR ARRAY ARCHITECTURE
DEVELOPMENT OF INNOVATIVE MECHANICAL FLEXIBLE SOLAR ARRAY ARCHITECTURE Bernard BOULANGER (1), Yannick BAUDASSÉ (1), François GUINOT (1), Laurent D ABRIGEON (1), Mikaël THIBAUDEAU (1), Marina HEIM (2),
More informationSolar & Electric Sailing Overview
Solar & Electric Sailing Overview KISS Technology Development Workshop (May 15-18, 2018) NASA Image NASA Image Jared Dervan NASA/MSFC Acknowledgments Les Johnson (MSFC Project Formulation Office) Bruce
More informationPreliminary Design Review: Loads, Structures, and Mechanisms. Michael Cunningham, Shimon Gewirtz, Rajesh Yalamanchili, Thomas Noyes
Preliminary Design Review: Loads, Structures, and Mechanisms Michael Cunningham, Shimon Gewirtz, Rajesh Yalamanchili, Thomas Noyes Crew Cabin Structure Height of ~3.7m from heat shield to top of the cone
More informationJonathan Fraser METEOR Project P07102 Environmental Test Stand Project Manager/Lead Engineer Detail Design Review Report
Jonathan Fraser METEOR Project P07102 Environmental Test Stand Project Manager/Lead Engineer Detail Design Review Report The project, P07102 Environmental Test Stand, is specifically involved in the design,
More informationKinematic Analysis of the Deployable Truss Structures for Space Applications
Kinematic Analysis of the Deployable Truss Structures for Space Applications Xu Yan 1 *, Guan Fu-ling 1, Zheng Yao 1, Zhao Mengliang 1, Zhejiang University, Hangzhou China Shanghai JiangNan Architectural
More informationGravitational Fields Review
Gravitational Fields Review 2.1 Exploration of Space Be able to: o describe planetary motion using Kepler s Laws o solve problems using Kepler s Laws o describe Newton s Law of Universal Gravitation o
More informationScott Bolton OPAG February 1, 2016
Scott Bolton OPAG February 1, 2016 Juno Status Launched August 2011 Earth flyby October 2013 Jupiter arrival July 4, 2016 Spacecraft is healthy and all instruments are working. Juno Science Juno Science
More informationRadiation: Lessons Learned
Radiation: Lessons Learned Scott Bolton Southwest Research Institute Insoo Jun Jet Propulsion Laboratory This document has been reviewed for export control and it does NOT contain controlled technical
More informationGC005 thru GC600. Wireless Load Cell. Features. Applications. General Description. Load Cell
Wireless Load Cell Features Standard single part line pull sizes ranging from 5,000 to 600,000 lb. All stainless frame and hardware Heavy duty construction from 17-4PH1150 stainless steel (17-4PH1025 on
More informationGeneration X. Attitude Control Systems (ACS) Aprille Ericsson Dave Olney Josephine San. July 27, 2000
Generation X Attitude Control Systems (ACS) Aprille Ericsson Dave Olney Josephine San July 27, 2000 ACS Overview Requirements Assumptions Disturbance Torque Assessment Component and Control Mode Recommendations
More informationPhysics Standard level Paper 1
Physics Standard level Paper 1 Tuesday 8 November 2016 (morning) 45 minutes Instructions to candidates Do not open this examination paper until instructed to do so. Answer all the questions. For each question,
More informationMarch 4, 2013 Eric P. Smith JWST Program Office
March 4, 2013 Eric P. Smith JWST Program Office 1 SIMPLIFIED SCHEDULE OTE = Optical Telescope Element OTIS = Optical Telescope + ISIM k months of project funded critical path (mission pacing) schedule
More informationPropulsion Technology Assessment: Science and Enabling Technologies to Explore the Interstellar Medium
Propulsion Technology Assessment: Science and Enabling Technologies to Explore the Interstellar Medium January 2015 Les Johnson / NASA MSFC / ED04 www.nasa.gov Mission Statement Interstellar Probe Mission:
More informationChapter 31 Maxwell s Equations and Electromagnetic Waves. Copyright 2009 Pearson Education, Inc.
Chapter 31 Maxwell s Equations and Electromagnetic Waves Units of Chapter 31 Changing Electric Fields Produce Magnetic Fields; Ampère s Law and Displacement Current Gauss s Law for Magnetism Maxwell s
More informationPhysics 218: Midterm#1
Physics 218: Midterm#1 February 25 th, 2015 Please read the instructions below, but do not open the exam until told to do so. Rules of the Exam: 1. You have 75 minutes to complete the exam. 2. Formulae
More informationLRO/CRaTER. Technical Interchange Meeting. LRO Mechanical Systems. Giulio Rosanova / /
LRO/CRaTER Technical Interchange Meeting LRO Mechanical Systems Giulio Rosanova / 543 301-286-5907 / Giulio.G.Rosanova@nasa.gov 1 LRO Baseline (Deployed 0n Orbit) High Gain Antenna IM Optical Bench /Radiator
More informationAPERTURE: A Precise, Extremely- large Reflective Telescope Using Re- configurable Elements Melville P. Ulmer/Northwestern University
APERTURE: A Precise, Extremely- large Reflective Telescope Using Re- configurable Elements Melville P. Ulmer/Northwestern University Concept Large mirrors with post deployment correction Used for both
More informationSAILING THE PLANETS: PLANETARY EXPLORATION FROM GUIDED BALLOONS. 7 th Annual Meeting of the NASA Institute for Advanced Concepts
SAILING THE PLANETS: PLANETARY EXPLORATION FROM GUIDED BALLOONS 7 th Annual Meeting of the NASA Institute for Advanced Concepts DR. ALEXEY PANKINE GLOBAL AEROSPACE CORPORATION SAILING THE PLANETS 1 MARS
More informationSpinning Satellites Examples. ACS: Gravity Gradient. ACS: Single Spin
Attitude Determination and Attitude Control Placing the telescope in orbit is not the end of the story. It is necessary to point the telescope towards the selected targets, or to scan the selected sky
More informationOHB System AG, Universitätsallee 27-29, Bremen, Germany, (2)
DESIGN AND DEVELOPMENT PLAN OF A TENTACLES BASED CLAMPING MECHANISM FOR ACTIVE DEBRIS REMOVAL 13 TH SYMPOSIUM ON ADVANCED SPACE TECHNOLOGIES IN ROBOTICS AND AUTOMATION Jan-Christian Meyer (1), Marc Scheper
More informationPhysics 12 Final Exam Review Booklet # 1
Physics 12 Final Exam Review Booklet # 1 1. Which is true of two vectors whose sum is zero? (C) 2. Which graph represents an object moving to the left at a constant speed? (C) 3. Which graph represents
More informationSF016: PAST YEAR PSPM QUESTIONS
GRAPH QUESTIONS PSPM I 005/006 NO. 9 9. An experiment was carried out to determine the Young s modulus of a metal wire of length 3.0 and diameter 0.8. A vernier scale was used to measure its extension.
More informationPreliminary Development of an Experimental Lightweight Pulsed Plasma Thruster for Solar Sail Attitude Control
Preliminary Development of an Experimental Lightweight Pulsed Plasma Thruster for Solar Sail Attitude Control Kevin Pryor, Bong Wie, and Pavlos Mikellides Arizona State University 18 th Annual AIAA/USU
More informationNovel Design Elements of the Space Technology 5 Mechanical Subsystem
Novel Design Elements of the Space Technology 5 Mechanical Subsystem Peter Rossoni NASA Goddard Space Flight Center, Greenbelt, MD, 301-286-5854, Peter.Rossoni-1@NASA.gov William McGill Swales Aerospace,
More informationElectroMagnetic Induction
ElectroMagnetic Induction Physics 1 What is E/M Induction? Electromagnetic Induction is the process of using magnetic fields to produce voltage, and in a complete circuit, a current. Michael Faraday first
More informationArgo. Voyage Through the Outer Solar System. Presentation to SBAG 12 January Candice Hansen (JPL) & Heidi B. Hammel (Space Science Institute)
Argo Voyage Through the Outer Solar System Presentation to SBAG 12 January 2009 Candice Hansen (JPL) & Heidi B. Hammel (Space Science Institute) Argo: New Frontiers 4 Mission Concept "A small-body explorer
More informationLunar Reconnaissance Orbiter Project. Cosmic Ray Telescope for the Effects of Radiation to Spacecraft Mechanical Interface Control Document
Revision B DraftA Effective Date: July 17, 2006 Expiration Date: July 17, 2011 Lunar Reconnaissance Orbiter Project Cosmic Ray Telescope for the Effects of Radiation to Spacecraft Mechanical Interface
More informationDeployment of an Interstellar Electromagnetic Acceleration System
Deployment of an Interstellar Electromagnetic Acceleration System Andrew Bingham Department of Mechanical and Aeronautical Engineering Clarkson University Phase I Fellows Meeting March 15-16, 2005 Atlanta,
More informationFree-Fall Acceleration
Objective To determine the acceleration due to gravity. Introduction Free-Fall Acceleration The position y of a particle moving along a straight line with a constant acceleration a is given by the following
More informationJames Webb Space Telescope (JWST)
James Webb Space Telescope (JWST) Engineering the Beginning US Frontiers of Engineering Conference Amy S. Lo JWST System Engineering Space-Based observation has enabled giant leaps in our understanding
More informationSolar Thermal Power System for Oxygen Production from Lunar Regolith
VG08-036 Solar Thermal Power System for Oxygen Production from Lunar Regolith Takashi Nakamura 1, Aaron D. Van Pelt 1, Robert J. Gustafson 2, and Larry Clark 3 1 Physical Sciences Inc. 2 Orbital Technologies
More informationa. What is the velocity of the electrons as they leave the accelerator?
1. An electron enters a uniform magnetic field of 0.23 T at a 45 angle to Determine the radius r and pitch p (distance between loops as shown below) of the electron s helical path assuming its speed is
More informationThe centroid of an area is defined as the point at which (12-2) The distance from the centroid of a given area to a specified axis may be found by
Unit 12 Centroids Page 12-1 The centroid of an area is defined as the point at which (12-2) The distance from the centroid of a given area to a specified axis may be found by (12-5) For the area shown
More informationHigh speed and quick response precise linear stage system using V-shape transducer ultrasonic motors
High speed and quick response precise linear stage system using V-shape transducer ultrasonic motors K. Asumi, T. Fujimura and M. K. Kurosawa Taiheiyo-cement Corporation, Japan Tokyo Institute of Technology,
More informationThe B612 Foundation Sentinel Mission. Ed Lu CEO, B612 Foundation
The B612 Foundation Sentinel Mission Ed Lu CEO, B612 Foundation The B612 Foundation Silicon Valley based nonprofit 501(c)3 Founded 2002 Mission is to protect humanity by preventing future asteroid impacts
More informationIntroduction of Small Solar Power Sail Demonstrator IKAROS
Introduction of Small Solar Power Sail Demonstrator IKAROS IKAROS Demonstration Team JAXA Space Exploration Center (JSPEC) Japan Aerospace Exploration Agency (JAXA) Overview of IKAROS IKAROS is a space
More informationD-SAT Simplified Magnetic Attitude Control
D-SAT Simplified Magnetic Attitude Control Warren K. Soh, Norhizam Hamzah, Ahmad Sabirin Arshad Astronautic Technology (M) Sdn. Bhd. (ATSB) Suite G1A, Enterprise 3, Technology Park Malaysia, Bukit Jalil
More informationBEOSAT (BRUNSWICK-EARTH-OBSERVATION-SATELLITE)
ABSTRACT BEOSAT (BRUNSWICK-EARTH-OBSERVATION-SATELLITE) Rolf Kluge Jörn Pfingstgräff ExperimentalRaumfahrt-InteressenGemeinschaft e.v., Germany r.kluge@tu-braunschweig.de j.pfingstgraeff@tu-braunschweig.de
More informationIn situ Investigations of the Local Interstellar Medium. Science Mission Technology, TRL
Science Mission Technology, TRL 1 Introduction Astrospheres are a ubiquitous phenomenon... LL Orionis Visible Hubble Astrosphere: The region in space influenced by the outflowing stellar wind and embedded
More information