List of All Rocket Launches from Esrange Space Center
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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. -
Sounding Rocket - Wikipedia, the Free Encyclopedia Page 1 of 4
Sounding rocket - Wikipedia, the free encyclopedia Page 1 of 4 Sounding rocket From Wikipedia, the free encyclopedia (Redirected from Sounding rockets) A sounding rocket, sometimes called a research rocket, is an instrument-carrying rocket designed to take measurements and perform scientific experiments during its sub-orbital flight. The origin of the term comes from nautical vocabulary, where to sound is to throw a weighted line from a ship into the water, to gauge the water's depth. Sounding in the rocket context is equivalent to taking a measurement.[1] The rockets are used to carry instruments from 50 to 1,500 kilometers[2] above the surface of the Earth, the altitude generally between weather balloons and satellites (the maximum altitude for balloons is about 40km and the minimum for satellites is approximately 120km).[3] Certain sounding rockets, such as the Black Brant X and XII, have an apogee between 1,000 and 1,500 kilometers; the maximum apogee of their class. Sounding rockets [1] often use military surplus rocket motors. NASA routinely flies A Black Brant XII being launched the Terrier Mk 70 boosted Improved Orion lofting 270–450 from Wallops Flight Facility. kilogram payloads into the exoatmospheric region between 100 and 200 kilometers.[4] Contents ■ 1 Design ■ 2 Advantages ■ 3 Research applications ■ 4 Operators and Programmes ■ 5 Other Uses ■ 6 See also ■ 7 References ■ 8 External links Design A common sounding rocket consists of a solid-fuel rocket motor and a science payload.[1] The freefall part of the flight is an elliptic trajectory with vertical major axis allowing the payload to appear to hover near its apogee.[3] The average flight time is less than 30 minutes, usually between five and 20 minutes. -
MORABA Sounding Rocket Launch Vehicles
MORABA Sounding Rocket Launch Vehicles Mobile Rocket Base German Aerospace Center Sounding Rocket Launch Vehicles 1.1. Introduction The research vehicles offered by MORABA have been used by a wide spectrum of payloads, differing in mass, complexity and transport requirements. In order to serve the needs of any payload and transport requirement, MORABA relies on a large portfolio of rocket motors that it uses in single stage as well as stacked configurations. MORABA constantly strives to enhance the portfolio of active rocket motors in order to improve its transport capacities or replace systems that run out of stock. Although the developments in liquid, gelled and hybrid propulsion are closely followed, the high power density, operational simplicity and safety of solid rocket motors have led to their exclusive use by MORABA so far. A large portion of the active portfolio is formed by motors with military heritage. These motors are conceded to MORABA or its partners from governments that tear down a fraction of their armory. As usually these motors have exceeded their shelf life, inspection and re-lifing efforts become necessary. Many successful missions prove the flight worthiness of these motors which are not least attractive due to their competitive price. The second group of the portfolio is made up by motors available from third parties. Here, MORABA is constantly evaluating potential candidates. A longstanding cooperation with the Brazilian Department of Aerospace Science and Technology (DCTA) has led to frequent use of its S31 and S30 rocket motor stages. At current, MORABA is also developing a solid motor stage with Bayern Chemie GmbH and acquiring some units of Magellan’s Black Brant V. -
NASA Sounding Rockets Annual Report 2019 at NASA Headquarters Who Approved These Missions As Excepted Activities During the Partial Government Shutdown
National Aeronautics andSpaceAdministration National Aeronautics NASA Sounding Rockets Annual Report 2019 at NASA Headquarters who approved these missions as excepted activities during the partial government shutdown. The second phase of this campaign featured two rockets for the Auroral Zone Upwelling Rocket Experiment (AZURE) mission, which produced spectacular images from the neutral wind measurement tracers that were released and glowed in the northern sky. CGI-Cusp continues in Fiscal Year 2020 with two planned NASA missions; Cusp Region EXperiment (C-REX) 2 launching from Andoya Space Center, and Cusp Heating Investigation (CHI) launching from Svalbard. For 2020 we are also continuing to work toward supporting south- ern hemisphere astrophysics missions from Australia. A new launch range, Equatorial Launch Australia (ELA), will be used for these missions supported by our mobile assets. The missions are currently manifested for a July 2020 launch window, and focus on UV and X-ray research. We heard from some of the hundreds of students we inspire every year: Message from the Chief Message Giovanni Rosanova “RockSat-X was a great opportunity for me to get experience build- ing a sounding rocket payload. Getting to learn from and network Chief, Sounding Rockets Program Office with engineers here at Wallops is an opportunity I will forever be grateful for.” Josh Loredo - Computer Science & Mathematics - The Sounding Rocket Program continued to reach for the heavens University of Kentucky in 2019. We launched 17 missions, from 5 launch sites around the globe, using 6 vehicle configurations and covering five different "Ever since I was a child I knew that my purpose was within the science disciplines. -
Sounding Rocket Program Handbook (SRPH)
Downloaded from http://www.everyspec.com Sounding Rocket Program Handbook (SRPH) Suborbital Projects and Operations Directorate Sounding Rockets ProgramOffice June 1, 1999 Goddard Space Flight Center National Aeronautics and Wallops Flight Facility Space Administration Wallops Island, Virginia 23337 Downloaded from http://www.everyspec.com Preface This Handbook describes the capabilities of the program, the design and technology applications to be considered, and the process NASA has established to integrate the customer (principal investigator/program user/scientist/experimenter) into the sounding rocket mission team to ensure the highest probability of a successful project. Neither the United States Government nor any person acting on the behalf of the Unites States Government assumes any liability resulting from the use of information contained in this document or warrants that the use will be free from privately owned rights. The use of a company name does not imply approval or recommendation of the product to the exclusion of others that may also be suitable. ii Downloaded from http://www.everyspec.com Sounding Rocket Program Handbook Table of Contents PREFACE .......................................................................II SECTION 1: NASA SOUNDING ROCKET PROGRAM........................... 2 1.1 INTRODUCTION ...................................................................................2 1.2 NASA ORGANIZATIONAL RESPONSIBILITIES ................................................1-3 1.3 SOUNDING ROCKET PROGRAM CUSTOMER’S -
Sounding Rocket Working Group
Sounding Rocket Working Group 21 January 2014 The attached documents contain technical data within the definition of the International Traffic in Arms Regulation, and are subject to the export control laws of the U.S. Government. Transfer of this data by any means to a foreign person, whether in the U.S. or abroad, without an export license or other approval from the U.S. Department of State, is prohibited. Similarly, publication or other release into the public domain constitutes an export and is not authorized, except as approved by the cognizant U.S. government department or agency. NSRP Briefing Outline • Programmatics - Eberspeaker/Schafer SRPO NSROC • Schedule Adherence - Eberspeaker • Success Criteria Guidelines - Ransone • Anomaly Status - Rosanova • Motors & Vehicle Systems - Brodell/Hesh/Hunter Surplus Peprgrine Brants Orioles FTS Caster • Annual Report & PI Questionnaire - Eberspeaker • Educational Activities - Eberspeaker/Koehler • Range Status - Ransone Wallops Pker WSMR Kwajalein Norway Australia • Technology Development - Rosanova / NSROC 2 SRPO Programmatic Eberspeaker The attached documents contain technical data within the definition of the International Traffic in Arms Regulation, and are subject to the export control laws of the U.S. Government. Transfer of this data by any means to a foreign person, whether in the U.S. or abroad, without an export license or other approval from the U.S. Department of State, is prohibited. Similarly, publication or other release into the public domain constitutes an export and is not authorized, except as approved by the cognizant U.S. government department or agency. June SRWG Findings 1. Strong Concern Regarding Program Vitality (Letter sent to NASA HQ) • The SRPO appreciates the support… 2. -
Final Environmental Impact Statement for the Sounding Rockets Program at Poker Flat Research Range (PFRR EIS)
CHAPTER 2 DESCRIPTION AND COMPARISON OF ALTERNATIVES This page intentionally left blank. 2. DESCRIPTION AND COMPARISON OF ALTERNATIVES This chapter describes the National Aeronautics and Space Administration’s Sounding Rockets Program, the proposed action, and the alternatives for the Poker Flat Research Range located near Fairbanks, Alaska. As discussed in Chapter 1, the National Aeronautics and Space Administration (NASA) is analyzing its continued use of the Poker Flat Research Range (PFRR) as part of the Sounding Rockets Program (SRP) in this Final Environmental Impact Statement for the Sounding Rockets Program at Poker Flat Research Range (PFRR EIS). Five alternatives, including a No Action Alternative, are being evaluated. Each of the alternatives considers two potential scenarios for future launches, which are: (1) a continuation of launches from PFRR in much the same manner as has been done in the past; and (2) a modification or end to future launches resulting from a non-issuance of authorizations from the U.S. Bureau of Land Management (BLM) and/or U.S. Fish and Wildlife Service (USFWS) for impacts on their lands. Under either authorization scenario, a key difference among the alternatives is the level of effort undertaken to locate and recover expended flight hardware from downrange lands. Two alternatives also incorporate restrictions in future launch trajectories. How this Chapter is Organized This chapter of the EIS is intended to provide the reader both an understanding of typical NASA sounding rocket operations at PFRR and the alternatives considered. Section 2.1 provides an overview of NASA sounding rocket operations at PFRR, including details of past and present launches and launch vehicles, PFRR facilities and infrastructure, and a discussion of typical flight and recovery activities. -
Sounding Rocket Program Handbook
Sounding Rocket Program Handbook Suborbital Projects and Operations Directorate Sounding Rockets Program Office National Aeronautics and Space Administration Goddard Space Flight Center Wallops Flight Facility Wallops Island, Virginia 23337 July 2001 Preface This Handbook describes the capabilities of the Sounding Rocket program, the design and technology applications used by that program, and the processes established to integrate the customer (principal investigator/program user/scientist/experimenter) into the mission team to ensure the highest probability of a successful project. Neither the United States Government nor any person acting on the behalf of the Unites States Government assumes any liability resulting from the use of information contained in this document or warrants that the use will be free from privately owned rights. The use of a company name does not imply approval or recommendation of the product to the exclusion of others that may also be suitable. i SOUNDING ROCKET PROGRAM HANDBOOK TABLE OF CONTENTS PREFACE SECTION 1: THE NASA SOUNDING ROCKET PROGRAM (NSRP) 1 1.1 THE PROGRAM: 1959 - THE PRESENT 1 1.2 NASA ORGANIZATIONAL RESPONSIBILITIES 2 1.2.1 PROGRAM MANAGEMENT 3 1.2.2 SOUNDING ROCKET WORKING GROUP (SRWG) 3 1.3 SOUNDING ROCKET PROGRAM CUSTOMER’S ROLE 3 1.3.1 PHILOSOPHY 3 1.3.2 PAYLOAD AND INSTRUMENTATION 4 1.4 SOUNDING ROCKET PROJECT SUPPORT ELEMENTS 4 1.4.1 PROGRAM-PROVIDED SUPPORT SERVICES 5 SECTION 2: THE SOUNDING ROCKET FLIGHT PROJECT 12 2.1 THE MISSION INITIATION CONFERENCE (MIC) 13 2.2 THE REQUIREMENTS -
Sounding Rockets 2016 Annual Report
National Aeronautics and Space Administration NASA Sounding Rockets Annual Report 2016 The Sounding Rockets Program also made world-class sci- ence discoveries over the past year. Our geospace missions continued to collect data to better understand the Sun-Earth interaction and space weather. The University of Miami Dif- fuse X-ray emission from the Local Galaxy (DXL) mission collected critical data that has helped scientists solve the questions of the origins on X-rays emanating in the Local Hot Bubble (LHB) that was generated by multiple, ancient supernova explosions that occurred in our region of space. The program once again push the boundaries of technol- ogy, not only for the program itself, but also for NASA as a whole. For example, we flew several technology demonstra- tion experiments for NASA's Space Technology Mission Directorate (STMD) Flight Opportunities Program (FOP). This included the RadPC, a computer system that uses a Phil Eberspeaker from the Chief Message novel architecture and off-the-shelf parts to increase flight Chief, Sounding Rockets Program Office computer reliability in the presence of high-energy radia- tion at a fraction of the cost of existing rad-hard computer Another year has passed, and the NASA Sounding Rockets systems. Another technology involved the VIP, a vibration Program has once again completed a wide variety of impres- isolation platform which will be used to reduce spacecraft sive scientific, educational, and technology demonstration disturbances during microgravity. We engaged in numerous missions. We launched eight missions from sites in Norway, other technology development efforts to enhance data trans- New Mexico and Virginia that carried science payloads to mission rates, more precisely deploy sub-payloads, enable study the Earth's near space environment, deep space ob- long range water recovery, and enable higher altitude flights. -
IAC-11-A2.5.9 Page 1 of 11 IAC-13-A2.5.10 DLR's MOBILE
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by Institute of Transport Research:Publications 64th International Astronautical Congress, Beijing, China. Copyright ©2013 by the International Astronautical Federation. All rights reserved. IAC-13-A2.5.10 DLR’S MOBILE ROCKET BASE – FLIGHT TICKETS FOR YOUR MICROGRAVITY EXPERIMENTS Andreas Stamminger Deutsches Zentrum für Luft- und Raumfahrt (DLR), Mobile Rocket Base, Oberpfaffenhofen, 82234 Wessling, Germany, Tel.: +49-8153-28-1231, Email: [email protected] Ludwig Altenbuchner Deutsches Zentrum für Luft- und Raumfahrt (DLR), Mobile Rocket Base, Oberpfaffenhofen, 82234 Wessling, Germany, Tel.: +49-8153-28-1457, Email: [email protected] Josef Ettl Deutsches Zentrum für Luft- und Raumfahrt (DLR), Mobile Rocket Base, Oberpfaffenhofen, 82234 Wessling, Germany, Tel.: +49-8153-28-2715, Email: [email protected] Marcus Hörschgen-Eggers Deutsches Zentrum für Luft- und Raumfahrt (DLR), Mobile Rocket Base, Oberpfaffenhofen, 82234 Wessling, Germany, Tel.: +49-8153-28-2172, Email: [email protected] Wolfgang Jung Deutsches Zentrum für Luft- und Raumfahrt (DLR), Mobile Rocket Base, Oberpfaffenhofen, 82234 Wessling, Germany, Tel.: +49-8153-28-2724, Email: [email protected] Peter Turner Deutsches Zentrum für Luft- und Raumfahrt (DLR), Mobile Rocket Base, Oberpfaffenhofen, 82234 Wessling, Germany, Tel.: +49-8153-28-2613, Email: [email protected] Mobile Rocket Base (MORABA), a section of DLR’s Space Operations and Astronaut Training Department fosters the national and international scientific community to prepare and implement sounding rocket and balloon borne experiments in the fields of aeronomy, astronomy, geophysics, hypersonic and especially microgravity research worldwide. In addition, satellite missions can be supported by mobile tracking radars for trajectory determination as well as with TT&C ground stations. -
NASA Sounding Rockets Program
https://ntrs.nasa.gov/search.jsp?R=20190025970 2019-08-31T14:17:11+00:00Z NASA Sounding Rockets Program Giovanni Rosanova Program Manager NASA Sounding Rockets Program 1 Sounding Rockets Program Office Organization Program Manager (Giovanni Rosanova) Deputy Program Manager (John Hickman) Business Technical Payload Vehicle Systems Safety and Manager Manager Systems Manager Mission NSROC COR Projects Projects Operations Operations Operations Manager (Chuck Brodell) Assurance (Julie Bloxom) Export Control Manager Manager Manager Manager Manager (Brian Hall) Manager (Carsell Milliner) (Libby West) (Gordon Marsh) (Nathan Empson) (Scott Bissett) (vacant) (Todd Thornes) Project Support Specialist (Valerie Jagow) Technology Grants and Admin Manager (Contractor) (Cathy Hesh) Resources Analyst Resources Analyst Embedded Embedded (Jennifer McIntyre) Reimbursables Mechanical Electrical (matrix) (Wyle Maddox) (matrix) Engineer Engineer (Josh Yacobucci) (Scott Hesh) (matrix) (matrix) 2 Nature of the NASA Sounding Rockets Program • Characteristics ‒Low cost o Part of the NASA Low Cost Access to Space (LCAS) program ‒ Quick turn around ‒ Rely on military surplus rocket motors as much as possible to reduce cost ‒ Acceptance of higher technical risk o Lower consequence Student and faculty members inspect o Higher probability of issues or failure their instrument prior to integration with ‒ Minimalistic project teams the university outreach payload RockSat-X ‒ Highly flexible and agile ‒ Non Mil‐Spec components ‒ Governed by NPR 7120.8 (Research and Technology)