Sounding Rocket Program Handbook
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Commercial Space Transportation Developments and Concepts: Vehicles, Technologies and Spaceports
Commercial Space Transportation 2006 Commercial Space Transportation Developments and Concepts: Vehicles, Technologies and Spaceports January 2006 HQ003606.INDD 2006 U.S. Commercial Space Transportation Developments and Concepts About FAA/AST About the Office of Commercial Space Transportation The Federal Aviation Administration’s Office of Commercial Space Transportation (FAA/AST) licenses and regulates U.S. commercial space launch and reentry activity, as well as the operation of non-federal launch and reentry sites, as authorized by Executive Order 12465 and Title 49 United States Code, Subtitle IX, Chapter 701 (formerly the Commercial Space Launch Act). FAA/AST’s mission is to ensure public health and safety and the safety of property while protecting the national security and foreign policy interests of the United States during commercial launch and reentry operations. In addition, FAA/AST is directed to encour- age, facilitate, and promote commercial space launches and reentries. Additional information concerning commercial space transportation can be found on FAA/AST’s web site at http://ast.faa.gov. Federal Aviation Administration Office of Commercial Space Transportation i About FAA/AST 2006 U.S. Commercial Space Transportation Developments and Concepts NOTICE Use of trade names or names of manufacturers in this document does not constitute an official endorsement of such products or manufacturers, either expressed or implied, by the Federal Aviation Administration. ii Federal Aviation Administration Office of Commercial Space Transportation 2006 U.S. Commercial Space Transportation Developments and Concepts Contents Table of Contents Introduction . .1 Significant 2005 Events . .4 Space Competitions . .6 Expendable Launch Vehicles . .9 Current Expendable Launch Vehicle Systems . .9 Atlas 5 - Lockheed Martin Corporation . -
Les Fusées-Sondes De Sud-Aviation
Les fusées-sondes de Sud-Aviation Jean-Jacques Serra Commission Histoire de la 3AF Origines : Centre national d'études des télécommunications (CNET) • Loi du 4 mai 1944, validée le 29 janvier 1945 • Demandes d'études - ministères (Guerre, Air, Marine), - Radiodiffusion française, - Comité d’action scientifique de la Défense nationale,... • Etudes sur la propagation radioélectrique plusieurs départements (Tubes et hyperfréquence, Transmission, Laboratoire national de radioélectricité) • Recherches sur la troposphère et sur l’ionosphère Programme spatial du CNET lancé en 1957 selon deux directions : • participation au lancement de fusées-sondes pour l’exploration de la haute atmosphère • traitement scientifique des données fournies par les signaux émis par les satellites artificiels Samedis de l'Histoire de la 3AF Les fusées-sondes de Sud Aviation 15/10/2011 - 2 Contexte : Fusées-sondes existantes Fusées du CASDN pour l'AGI : • Véronique AGI : dérivée des Véronique N et NA (1952-1954) 60 kg à 210 km d'altitude • Monica IV et V : dérivées des Monica I à III (1955-1956) 15 kg à 80 km ou 140 km d'altitude Fusées de l'ONERA utilisées par le CEA : • Daniel : dérivé d'Ardaltex (1957-1959) 15 kg à 125 km d'altitude • Antarès : dérivé de l'engin d'essais de rentrée (1959-1961) 35 kg à 280 km d'altitude Samedis de l'Histoire de la 3AF Les fusées-sondes de Sud Aviation 15/10/2011 - 3 Définition des besoins du CNET Envoi d'une charge utile de 32 kg à 80 km, 120 km, 400 km et 1000 km d'altitude • fusées commandées à Sud Aviation • unité mobile construite -
Suborbital Platforms and Range Services (SPARS)
Suborbital Capabilities for Science & Technology Small Missions Workshop @ Johns Hopkins University June 10, 2019 Mike Hitch, Giovanni Rosanova Goddard Space Introduction Flight Center AGENDAWASP OPIS ▪ Purpose ▪ History & Importance of Suborbital Carriers to Science ▪ Suborbital Platforms ▪ Sounding Rockets ▪ Balloons (brief) ▪ Aircraft ▪ SmallSats ▪ WFF Engineering ▪ Q & A P-3 Maintenance 12-Jun-19 Competition Sensitive – Do Not Distribute 2 Goddard Space Purpose of the Meeting Flight Center Define theWASP OPISutility of Suborbital Carriers & “Small” Missions ▪ Sounding rockets, balloons and aircraft (manned and unmanned) provide a unique capability to scientists and engineers to: ▪ Allow PIs to enhance and advance technology readiness levels of instruments and components for very low relative cost ▪ Provide PIs actual science flight opportunities as a “piggy-back” on a planned mission flight at low relative cost ▪ Increase experience for young and mid-career scientists and engineers by allowing them to get their “feet wet” on a suborbital mission prior to tackling the much larger and more complex orbital endeavors ▪ The Suborbital/Smallsat Platforms And Range Services (SPARS) Line Of Business (LOB) can facilitate prospective PIs with taking advantage of potential suborbital flight opportunities P-3 Maintenance 12-Jun-19 Competition Sensitive – Do Not Distribute 3 Goddard Space Value of Suborbital Research – What’s Different? Flight Center WASP OPIS Different Risk/Mission Assurance Strategy • Payloads are recovered and refurbished. • Re-flights are inexpensive (<$1M for a balloon or sounding rocket vs >$10M - 100M for a ELV) • Instrumentation can be simple and have a large science impact! • Frequent flight opportunities (e.g. “piggyback”) • Development of precursor instrument concepts and mature TRLs • While Suborbital missions fully comply with all Agency Safety policies, the program is designed to take Higher Programmatic Risk – Lower cost – Faster migration of new technology – Smaller more focused efforts, enable Tiger Team/incubator experiences. -
Sounding Rockets 2017 Annual Report
National Aeronautics and Space Administration NASA Sounding Rockets Annual Report 2017 particle energy measurements. Where once five or six free flying subpayloads were possible, now twenty or more are feasible. Astrophysicists are always wanting to collect more photons to enhance scientific return. This dictates a need for either larger diameter payloads to accommodate larger mirrors, or longer obser- vation times – and usually both. Astrophysics missions have, to a large extent, been limited to flying from White Sands Missile Range in New Mexico due to the requirement to recover the instruments for re-flight. Longer flights require higher apogees, which gener- ally dictate the need for ranges with larger impact areas. Larger launch ranges usually require flight over the ocean. The program is developing new water recovery technologies to enable such missions at a cost that is commensurate with the low-cost nature of the program. The new system includes a hydrodynamic wedge to reduce impact loads and sealed sections to protect the science instruments and expensive support systems such as telemetry and attitude control systems. The trick is, each of these systems needs to have some sort of exposure to the outside environment during the scientific data period, yet be sealed when they impact the ocean. While ocean recovery has been done for essentially the entire life of the program, it has involved relatively basic systems that offered few Phil Eberspeaker from the Chief Message engineering challenges. Now telescopes, telemetry systems, attitude Chief, Sounding Rockets Program Office controls systems, and even the recovery systems themselves need to be protected so they can be reflow on future missions. -
Performance Modelling and Simulation of a 100 Km Hybrid Sounding Rocket
PERFORMANCE MODELLING AND SIMULATION OF A 100 KM HYBRID SOUNDING ROCKET Fiona Kay Leverone Submitted in fulfilment of the academic requirements for the degree of Master of Science in Mechanical Engineering, College of Agriculture, Engineering and Science, University of KwaZulu-Natal Supervisor: Mr Michael Brooks Co-Supervisor: Mr Jean-François Pitot de la Beaujardiere Co-Supervisor: Prof Lance Roberts December 2013 2. DECLARATION 1 - PLAGIARISM I, Fiona Leverone, declare that 1. The research reported in this thesis, except where otherwise indicated, is my original research. 2. This thesis has not been submitted for any degree or examination at any other university. 3. This thesis does not contain other persons’ data, pictures, graphs or other information, unless specifically acknowledged as being sourced from other persons. 4. This thesis does not contain other persons’ writing, unless specifically acknowledged as being sourced from other researchers. Where other written sources have been quoted, then: a. Their words have been re-written but the general information attributed to them has been referenced b. Where their exact words have been used, then their writing has been placed inside quotation marks, and referenced. 5. This thesis does not contain text, graphics or tables copied and pasted from the Internet, unless specifically acknowledged, and the source being detailed in the thesis and in the References sections. Signed ________________________ Date ___________ Miss Fiona Leverone As the candidate’s supervisor I have approved this dissertation for submission. Signed ________________________ Date ___________ Mr. Michael Brooks As the candidates co-supervisor I have approved this dissertation for submission. Signed ________________________ Date ___________ Mr. -
What's Inside... in Brief
National Aeronautics and Space Administration What’s inside... 2 Features 5 Integration and Testing 4 1 3 2 2015 6 Picture Place 7 Other News 8 Schedule & Miscellanea Sounding Rockets Program Office 46.012 UO Koehler - RockSat-X was succesfully launched In Brief... from Wallops Island on August 12, 2015. The new Black Brant Mk 4 vehicle will fly for the first time in October 2015 from Wallops Island. The payload carries several technology test experi- ments and instruments. Payload teams are preparing for the coming Norway campaign. Two rockets will be launched from Andoya with the launch window opening on November 27. The Multiple User Suborbital Instru- ment Carrier (MUSIC) payload will be launched from Wallops Island in Oc- tober on a Terrier-Improved Malemute rocket. The sounding rockets program will cel- ebrate 45-years at Wallops on Novem- ber 30, 2015. More on page 7. A very busy flight schedule is in prog- ress. The Sounding Rockets Program has 11 missions on schedule during the Students from Hawaii with their experiment after the successful flight. period September through November. The 46.012 UO RockSat-X mission was launched from Wallops Island, VA on Au- Three have been successfully complet- gust 12, 2015. RockSat-X is the most advanced of three student flight programs ed and eight remain. managed by Colorado Space Grant Consortium and supported by NASA. RockSat- X provides participating University faculty and students an opportunity to build, RockSat-X continued... test and fly an experiment of their own University Of Hawaii Community College design onboard a Terrier-Improved System University of Nebraska Lincoln (UNL) Malemute sounding rocket and in- Project Imua The experiment from the University of cludes full featured sounding rocket The primary mission goal for Project Nebraska Lincoln compared buoyant support systems, such as telemetry, Imua is to encourage UHCC students to convection on the ground in the pres- attitude control and recovery. -
Space Planes and Space Tourism: the Industry and the Regulation of Its Safety
Space Planes and Space Tourism: The Industry and the Regulation of its Safety A Research Study Prepared by Dr. Joseph N. Pelton Director, Space & Advanced Communications Research Institute George Washington University George Washington University SACRI Research Study 1 Table of Contents Executive Summary…………………………………………………… p 4-14 1.0 Introduction…………………………………………………………………….. p 16-26 2.0 Methodology…………………………………………………………………….. p 26-28 3.0 Background and History……………………………………………………….. p 28-34 4.0 US Regulations and Government Programs………………………………….. p 34-35 4.1 NASA’s Legislative Mandate and the New Space Vision………….……. p 35-36 4.2 NASA Safety Practices in Comparison to the FAA……….…………….. p 36-37 4.3 New US Legislation to Regulate and Control Private Space Ventures… p 37 4.3.1 Status of Legislation and Pending FAA Draft Regulations……….. p 37-38 4.3.2 The New Role of Prizes in Space Development…………………….. p 38-40 4.3.3 Implications of Private Space Ventures…………………………….. p 41-42 4.4 International Efforts to Regulate Private Space Systems………………… p 42 4.4.1 International Association for the Advancement of Space Safety… p 42-43 4.4.2 The International Telecommunications Union (ITU)…………….. p 43-44 4.4.3 The Committee on the Peaceful Uses of Outer Space (COPUOS).. p 44 4.4.4 The European Aviation Safety Agency…………………………….. p 44-45 4.4.5 Review of International Treaties Involving Space………………… p 45 4.4.6 The ICAO -The Best Way Forward for International Regulation.. p 45-47 5.0 Key Efforts to Estimate the Size of a Private Space Tourism Business……… p 47 5.1. -
The Annual Compendium of Commercial Space Transportation: 2017
Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2017 January 2017 Annual Compendium of Commercial Space Transportation: 2017 i Contents About the FAA Office of Commercial Space Transportation The Federal Aviation Administration’s Office of Commercial Space Transportation (FAA AST) licenses and regulates U.S. commercial space launch and reentry activity, as well as the operation of non-federal launch and reentry sites, as authorized by Executive Order 12465 and Title 51 United States Code, Subtitle V, Chapter 509 (formerly the Commercial Space Launch Act). FAA AST’s mission is to ensure public health and safety and the safety of property while protecting the national security and foreign policy interests of the United States during commercial launch and reentry operations. In addition, FAA AST is directed to encourage, facilitate, and promote commercial space launches and reentries. Additional information concerning commercial space transportation can be found on FAA AST’s website: http://www.faa.gov/go/ast Cover art: Phil Smith, The Tauri Group (2017) Publication produced for FAA AST by The Tauri Group under contract. NOTICE Use of trade names or names of manufacturers in this document does not constitute an official endorsement of such products or manufacturers, either expressed or implied, by the Federal Aviation Administration. ii Annual Compendium of Commercial Space Transportation: 2017 GENERAL CONTENTS Executive Summary 1 Introduction 5 Launch Vehicles 9 Launch and Reentry Sites 21 Payloads 35 2016 Launch Events 39 2017 Annual Commercial Space Transportation Forecast 45 Space Transportation Law and Policy 83 Appendices 89 Orbital Launch Vehicle Fact Sheets 100 iii Contents DETAILED CONTENTS EXECUTIVE SUMMARY . -
General Disclaimer One Or More of the Following
https://ntrs.nasa.gov/search.jsp?R=19700024621 2020-03-23T18:22:24+00:00Z General Disclaimer One or more of the Following Statements may affect this Document This document has been reproduced from the best copy furnished by the organizational source. It is being released in the interest of making available as much information as possible. This document may contain data, which exceeds the sheet parameters. It was furnished in this condition by the organizational source and is the best copy available. This document may contain tone-on-tone or color graphs, charts and/or pictures, which have been reproduced in black and white. This document is paginated as submitted by the original source. Portions of this document are not fully legible due to the historical nature of some of the material. However, it is the best reproduction available from the original submission. Produced by the NASA Center for Aerospace Information (CASI) r JULY 1969 WORLD DATA CENTER A Rockets and Satellites CATALOGUE OF DATA 1 JANUARY--30 JUNE 1%9 wa ^^acc...... 3 ^^ 1 0a-339 32 — r woo,,,,q • da Imam jMASA CR QI! {^ Ot AQ Ni1N^ KA^q I CATALOGUE OF DATA IN WORLD DATA CENTER A Rockets and satellites Data Received by WDC-A during the period 1 January — 30 June 1969 World Data Center A Rockets and Satellites Cude 601 Goddard Space Flight Center Greenbelt, Marylsnd, U.S.A. 20771 July 1969 Q PAG8 BtA6tK NO? RUED. INTRODUCTION World Data Centers conduct international exchange of geophysical observations in accordance with the principles set forth by the International Council of Scientific Unions (ICSU'). -
Desind Finding
NATIONAL AIR AND SPACE ARCHIVES Herbert Stephen Desind Collection Accession No. 1997-0014 NASM 9A00657 National Air and Space Museum Smithsonian Institution Washington, DC Brian D. Nicklas © Smithsonian Institution, 2003 NASM Archives Desind Collection 1997-0014 Herbert Stephen Desind Collection 109 Cubic Feet, 305 Boxes Biographical Note Herbert Stephen Desind was a Washington, DC area native born on January 15, 1945, raised in Silver Spring, Maryland and educated at the University of Maryland. He obtained his BA degree in Communications at Maryland in 1967, and began working in the local public schools as a science teacher. At the time of his death, in October 1992, he was a high school teacher and a freelance writer/lecturer on spaceflight. Desind also was an avid model rocketeer, specializing in using the Estes Cineroc, a model rocket with an 8mm movie camera mounted in the nose. To many members of the National Association of Rocketry (NAR), he was known as “Mr. Cineroc.” His extensive requests worldwide for information and photographs of rocketry programs even led to a visit from FBI agents who asked him about the nature of his activities. Mr. Desind used the collection to support his writings in NAR publications, and his building scale model rockets for NAR competitions. Desind also used the material in the classroom, and in promoting model rocket clubs to foster an interest in spaceflight among his students. Desind entered the NASA Teacher in Space program in 1985, but it is not clear how far along his submission rose in the selection process. He was not a semi-finalist, although he had a strong application. -
Space Wales Brochure Directory Capability Matrix (Lowres)
WALES A SUSTAINABLE SPACE NATION BROCHURE, DIRECTORY & CAPABILITY MATRIX SPACE WALES Wales - A Sustainable Space Nation 03 Space Wales Leadership Group 08 WASP & Academia 10 Research Centres & Catapults 11 RPAS and T&E in Wales 12 Capability Matrix 14 Company Directory 18 02 SPACE WALES WALES A SUSTAINABLE SPACE NATION Wales, with a population of 3 million people, totals around 5% of the UK populace. In the aerospace sector Wales has around 10% of the overall UK workforce and arguably punches above its weight. When it comes to the space sector Wales has only around 1% of the overall UK personnel and so there is a huge opportunity for growth in a sector which is growing significantly. The UK space sector has set a target of achieving a 10% share of the predicted £400 billion per annum global space market in 2030. A 5% share of this for Wales would equate to £2 billion per year and this is a realisable target which we aim to achieve and will work to exceed. Currently there are around 5000 satellites circling the earth in various orbits. Only 2,000 of these are operational. If OneWeb, Starlink and other potential networks continue with their projected growth that number could increase by a massive 4,500% in the next five years! Demand for data is on the increase, and launching satellites that offer broadband internet service will help to drive down the cost of that data. Reusable rockets and satellites will also help drive down costs and so too will the mass-production of satellites and the development of satellite technology. -
Failures in Spacecraft Systems: an Analysis from The
FAILURES IN SPACECRAFT SYSTEMS: AN ANALYSIS FROM THE PERSPECTIVE OF DECISION MAKING A Thesis Submitted to the Faculty of Purdue University by Vikranth R. Kattakuri In Partial Fulfillment of the Requirements for the Degree of Master of Science in Mechanical Engineering August 2019 Purdue University West Lafayette, Indiana ii THE PURDUE UNIVERSITY GRADUATE SCHOOL STATEMENT OF THESIS APPROVAL Dr. Jitesh H. Panchal, Chair School of Mechanical Engineering Dr. Ilias Bilionis School of Mechanical Engineering Dr. William Crossley School of Aeronautics and Astronautics Approved by: Dr. Jay P. Gore Associate Head of Graduate Studies iii ACKNOWLEDGMENTS I am extremely grateful to my advisor Prof. Jitesh Panchal for his patient guidance throughout the two years of my studies. I am indebted to him for considering me to be a part of his research group and for providing this opportunity to work in the fields of systems engineering and mechanical design for a period of 2 years. Being a research and teaching assistant under him had been a rewarding experience. Without his valuable insights, this work would not only have been possible, but also inconceivable. I would like to thank my co-advisor Prof. Ilias Bilionis for his valuable inputs, timely guidance and extremely engaging research meetings. I thank my committee member, Prof. William Crossley for his interest in my work. I had a great opportunity to attend all three courses taught by my committee members and they are the best among all the courses I had at Purdue. I would like to thank my mentors Dr. Jagannath Raju of Systemantics India Pri- vate Limited and Prof.