Launch Services Overview to Nasa Advisory Council
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Preface Patrick Besha, Editor Alexander Macdonald, Editor in The
EARLY DRAFT - NASAWATCH.COM/SPACEREF.COM Preface Patrick Besha, Editor Alexander MacDonald, Editor In the next decade, NASA will seek to expand humanity’s presence in space beyond the International Space Station in low-Earth orbit to a new habitation platform orbiting the moon. By the late 2020’s, astronauts will live and work far deeper in space than ever before. The push to cis-lunar orbit is part of a stepping-stone approach to extend our reach to Mars and beyond. This decision to explore ever farther destinations is a familiar pattern in the history of American space exploration. Another major pattern with historical precedent is the transition from public sector exploration to private sector commercialization. After the government has developed and demonstrated a capability in space, whether it be space-based communications or remote sensing, the private sector has realized its market potential. As new companies establish a presence, the government withdraws from the market. In 2015, we are once again at a critical stage in the development of space. The most successful long-term human habitation in space, orbiting the Earth continuously since 1998, is the International Space Station. Currently at the apex of its capabilities and the pinnacle of state-of-the-art space systems, it was developed through the investments and labors of over a dozen nations and is regularly re-supplied by cargo delivery services. Its occupants include six astronauts and numerous other organisms from Earth’s ecosystems from bacteria to plants to rats. Research is conducted on the spacecraft from hundreds of organizations worldwide ranging from academic institutions to large industrial companies and from high-tech start-ups to high-school science classes. -
Cape Canaveral Air Force Station Support to Commercial Space Launch
The Space Congress® Proceedings 2019 (46th) Light the Fire Jun 4th, 3:30 PM Cape Canaveral Air Force Station Support to Commercial Space Launch Thomas Ste. Marie Vice Commander, 45th Space Wing Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Ste. Marie, Thomas, "Cape Canaveral Air Force Station Support to Commercial Space Launch" (2019). The Space Congress® Proceedings. 31. https://commons.erau.edu/space-congress-proceedings/proceedings-2019-46th/presentations/31 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress® Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Cape Canaveral Air Force Station Support to Commercial Space Launch Colonel Thomas Ste. Marie Vice Commander, 45th Space Wing CCAFS Launch Customers: 2013 Complex 41: ULA Atlas V (CST-100) Complex 40: SpaceX Falcon 9 Complex 37: ULA Delta IV; Delta IV Heavy Complex 46: Space Florida, Navy* Skid Strip: NGIS Pegasus Atlantic Ocean: Navy Trident II* Black text – current programs; Blue text – in work; * – sub-orbital CCAFS Launch Customers: 2013 Complex 39B: NASA SLS Complex 41: ULA Atlas V (CST-100) Complex 40: SpaceX Falcon 9 Complex 37: ULA Delta IV; Delta IV Heavy NASA Space Launch System Launch Complex 39B February 4, 2013 Complex 46: Space Florida, Navy* Skid Strip: NGIS Pegasus Atlantic Ocean: Navy Trident II* Black text – current programs; -
Launch Vehicle Payload Envelope Analysis
CC BY-SA 4.0: Open Source Satellite 2021 Payload Envelope Envelope Payload Launch Vehicle Vehicle Launch Rich Tait, Collaborator OSSAT Analysis June 2021 June Contents Why are launcher envelopes important? Launch vehicles Envelopes Tools Further questions or want to get involved? : SA 4.0 SA - CC BY CC 2021 Satellite OpenSource Why are Launcher Envelopes Important? • Spacecraft experience the harshest mechanical environment during launch. • The mechanical environment can be described across several envelopes: • Quasi-Static Loads • Random Vibration • Acoustic • Shock • Envelopes feed the preliminary design and verification of spacecraft. : SA 4.0 SA - CC BY CC 2021 Satellite OpenSource Launch Vehicles • The analysis extends to the following launch vehicles: • Space X Falcon 9 • Rocket Labs Electron • Virgin Orbit Launcher One • Firefly Alpha • ABL RS1 • Soyuz • ArianeSpace Vega C • Envelopes have been overlayed to allow an overall envelope to be defined for the OSSAT solution. : SA 4.0 SA - CC BY CC 2021 Satellite OpenSource Quasi Static Loads • Combination of steady state and low frequency loads. • Mainly concern the primary structure. • Includes handling loads. : : SA 4.0 SA - SA 4.0 SA - CC BY CC 2021 Satellite OpenSource CC BY CC Satellite Open Source 2021 CC BY BY-SA-SA 4.0 4.0: : Open Source Source Satellite Satellite 2021 2021 • • Random Vibration Random the the launch. intensity overallof gives the GRMS launches. repeatable between Statistically CC BY BY-SA-SA 4.0 4.0: : Open Source Source Satellite Satellite 2021 2021 • • Acoustic the the launch. intensity overallof gives the OASPL the spacecraft. exterior panels of on the incident Acoustic are loads CC BY BY-SA-SA 4.0 4.0: : Open Source Source Satellite Satellite 2021 2021 • Shock Loads Shock payload separation. -
Space Coast Is Getting Busy: 6 New Rockets Coming to Cape Canaveral, KSC
4/16/2019 Space Coast is getting busy: 6 new rockets coming to Cape Canaveral, KSC Space Coast is getting busy: 6 new rockets coming to Cape Canaveral, Kennedy Space Center Emre Kelly, Florida Today Published 4:04 p.m. ET April 11, 2019 | Updated 7:53 a.m. ET April 12, 2019 COLORADO SPRINGS, Colo. – If schedules hold, the Space Coast will live up to its name over the next two years as a half-dozen new rockets target launches from sites peppered across the Eastern Range. Company, government and military officials here at the 35th Space Symposium, an annual space conference, have reaffirmed their plans to launch rockets ranging from more traditional heavy-lift behemoths to smaller vehicles that take advantage of new manufacturing technologies. Even if some of these schedules slip, at least one thing is apparent to several spaceflight experts here: The Eastern Range is seeing an unprecedented growth in commercial space companies and efforts. Space Launch System: 2020 NASA's Space Launch System rocket launches from Kennedy Space Center's pad 39B in this rendering by the agency. (Photo: NASA) NASA's long-awaited SLS, a multibillion-dollar rocket announced in 2011, is slated to become the most powerful launch vehicle in history if it can meet a stringent late 2020 deadline. The 322-foot-tall rocket is expected to launch on its first flight – Exploration Mission 1 – from Kennedy Space Center with an uncrewed Orion capsule for a mission around the moon, which fits in with the agency's wider goal of putting humans on the surface by 2024. -
Redalyc.Status and Trends of Smallsats and Their Launch Vehicles
Journal of Aerospace Technology and Management ISSN: 1984-9648 [email protected] Instituto de Aeronáutica e Espaço Brasil Wekerle, Timo; Bezerra Pessoa Filho, José; Vergueiro Loures da Costa, Luís Eduardo; Gonzaga Trabasso, Luís Status and Trends of Smallsats and Their Launch Vehicles — An Up-to-date Review Journal of Aerospace Technology and Management, vol. 9, núm. 3, julio-septiembre, 2017, pp. 269-286 Instituto de Aeronáutica e Espaço São Paulo, Brasil Available in: http://www.redalyc.org/articulo.oa?id=309452133001 How to cite Complete issue Scientific Information System More information about this article Network of Scientific Journals from Latin America, the Caribbean, Spain and Portugal Journal's homepage in redalyc.org Non-profit academic project, developed under the open access initiative doi: 10.5028/jatm.v9i3.853 Status and Trends of Smallsats and Their Launch Vehicles — An Up-to-date Review Timo Wekerle1, José Bezerra Pessoa Filho2, Luís Eduardo Vergueiro Loures da Costa1, Luís Gonzaga Trabasso1 ABSTRACT: This paper presents an analysis of the scenario of small satellites and its correspondent launch vehicles. The INTRODUCTION miniaturization of electronics, together with reliability and performance increase as well as reduction of cost, have During the past 30 years, electronic devices have experienced allowed the use of commercials-off-the-shelf in the space industry, fostering the Smallsat use. An analysis of the enormous advancements in terms of performance, reliability and launched Smallsats during the last 20 years is accomplished lower prices. In the mid-80s, a USD 36 million supercomputer and the main factors for the Smallsat (r)evolution, outlined. -
Falcon Heavy
Schaub 5:00 L04 Disclaimer: This paper partially fulfills a writing requirement for the first year (freshman) engineering students at the University of Pittsburgh Swanson School of Engineering. This paper is a student paper, not professional paper. This paper is based on publicly available information and may not provide complete analyses of all relevant data. If this paper is used for any purpose other than this author`s partial fulfillment of a writing requirement for first year (freshman) engineering students at the University of Pittsburgh Swanson School of Engineering, users are doing so at their own risk. FALCON HEAVY Zoë Neal ([email protected]) SPACEX order to finish the mission the vehicle was set out to SpaceX is a private space exploration do. company that designs and manufactures various Named after its use of nine first stage launch technologically advanced spacecraft and launch engineers, this is the world’s first partially reusable vehicles under the direction of co-founder and rocket [1]. It is comprised of three separate parts. CEO, Elon Musk [1]. The company was founded in The first stage is comprised of two boosters and the 2002 with the intent of advancing space exploration second stage is rocket itself. The Falcon 9 Full technology to achieve their ultimate goal of Thrust can lift cargo up to 50,300 pounds to low enabling humans to live on other planets. They are Earth orbit. That is the equivalent of sending a the first private company to return a spacecraft from sailboat, a greyhound bus, and a monster truck to an low-Earth orbit and are the first to use an orbital altitude of 1,200 miles. -
Connecticut Daily Campus I Serving Storrs Since 1896 V^»
Connecticut Daily Campus I Serving Storrs Since 1896 v^» VOL. CXVL No. 35 STORRS. CONNECTICUT THURSDAY, NOVEMBER 1, 1962 Increasing Shelters: Standards Lowered In reaction to the Cuban crisis, ately in initial radiation, heat, the office of Civil Defense has re- and blast. The remaining ten per quested that civil defense prepara- tions be speeded up. It called for cent shows up later as fine radia- nearly doubling the amount of ation dust particles. Eventually shelter space available by lower- they fall to earth. ing Hie standards now required Within the local area surround- for shielding from radiation. ing the target, roughly 80 per New Ruling cent of the falout will descend to According to the State Civil De- the ground in a matter of hours. fense Director, Captain William L. Schatzman, this lowering of The remainnig 20 per cent will Standards will "work out very circle the globe and may take well." He noted that with the new months or even years to fall. ruling, more people will be shield- Alway A Threat ed from the danger of a nuclear blast. Captain Schatzman pointed Fallout shelters are needed now out that safety in case of radio- as much as ever, according to active fallout will not be lessened Capt. Schatzman. He referred to but it might reduce the chances the trouble spots in Berlin. South- for survival in cases of a close east Asia and Cuba. "We should fire flash. "However, it's the only! thing we have," he added. always be prepared." he said. George F. Robinson, the Civilj "There is always a threat." Defense Director for the Town of i Mr. -
FIREFLY ALPHA PAYLOAD USER GUIDE Version 1 July 2015 FF-0005001 - Alpha 1.0 Payload Users Guide Rev 01 P a G E | 2
FIREFLY ALPHA PAYLOAD USER GUIDE Version 1 July 2015 FF-0005001 - Alpha 1.0 Payload Users Guide Rev 01 P a g e | 2 CONTACT INFORMATION Please contact Maureen Gannon with enquiries into the suitability of the Alpha Launch Vehicle for your mission. Maureen Gannon Vice President, Business Development Firefly Space Systems 1320 Arrow Point Drive Cedar Park, TX 78613 Phone: 512-234-3700 Fax: 877-318-8560 Email: [email protected] Web: www.fireflyspace.com Intellectual Property Designation. This document contains technical data that is Firefly proprietary. Export Control Designation. This document does not contain technical data subject to ITAR/EAR restrictions. © 2015 Firefly Space Systems, Inc. FF-0005001 - Alpha 1.0 Payload Users Guide Rev 01 P a g e | 3 REVISION HISTORY Revision Date By Notes 1 July 2015 Initial Release Intellectual Property Designation. This document contains technical data that is Firefly proprietary. Export Control Designation. This document does not contain technical data subject to ITAR/EAR restrictions. © 2015 Firefly Space Systems, Inc. FF-0005001 - Alpha 1.0 Payload Users Guide Rev 01 P a g e | 4 TABLE OF CONTENTS 1 Introduction ..........................................................................................................................8 1.1 Company Description .......................................................................................................... 8 1.2 Alpha Vehicle Overview ..................................................................................................... -
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. -
IMS Infrasound Records of Announced Rocket Launches
SnT2017 T1.1-P10 Disclaimer IMS Infrasound Records of Announced Rocket Launches The views expressed on this poster are those Tatiana Medinskaya, Paulina Bittner, Paul Polich, Pierrick Mialle, Jane Gore of the author and do not necessarily reflect the view of the CTBTO CTBTO Prep Com, Vienna International Centre, Austria. e-mail: [email protected] In 19 cases the launch pad was within the confidence ellipse (area in ABSTRACT which an event takes place with probability of 90%) associated to event CONSISTENCY OF INFRASOUND RECORDS Infrasound technology as part of the verification regime plays a location, in 4 cases event time differed by more than 20 minutes from To demonstrate consistency of infrasound signal signatures we checked IMS stations significant role in monitoring compliance with the Comprehensive the actual time of the launch. Therefore the epicentre significantly records of Soyuz rocket launches from Baikonur Cosmodrome. It is the largest and oldest Test Ban Treaty (CTBT). Low frequency acoustic waves under shifted from the launch location. For 5 launches some distinct events spaceport in the world located at the southern Kazakhstan and mostly used by favourable conditions can propagate thousands of kilometres until along the flight trajectory were registered in addition to signals Roskosmos. The closest IMS station is I31KZ (Aktubinsk, Kazakhstan) at the west from they arrive at infrasound arrays of the International Monitoring supposedly related to the liftoffs. the spaceport. The flight trajectory goes to the east towards IMS station I46RU (Zalesovo, System (IMS). Recorded data are transmitted to the International Russia). Data Centre (IDC) and used for detection and characterization of This study is aimed to inspect infrasound signal signatures and to atmospheric events. -
Small Launchers in a Pandemic World - 2021 Edition of the Annual Industry Survey
SSC21- IV-07 Small Launchers in a Pandemic World - 2021 Edition of the Annual Industry Survey Carlos Niederstrasser Northrop Grumman Corporation 45101 Warp Drive, Dulles, VA 20166 USA; +1.703.406.5504 [email protected] ABSTRACT Even with the challenges posed by the world-wide COVID pandemic, small vehicle "Launch Fever" has not abated. In 2015 we first presented this survey at the AIAA/USU Conference on Small Satellites1, and we identified twenty small launch vehicles under development. By mid-2021 ten vehicles in this class were operational, 48 were identified under development, and a staggering 43 more were potential new entrants. Some are spurred by renewed government investment in space, such as what we see in the U.K. Others are new commercial entries from unexpected markets such as China. All are inspired by the success of SpaceX and the desire to capitalize on the perceived demand caused by the mega constellations. In this paper we present an overview of the small launch vehicles under development today. When available, we compare their capabilities, stated mission goals, cost and funding sources, and their publicized testing progress. We also review the growing number of entrants that have dropped out since we first started this report. Despite the COVID-19 pandemic, one system became operational in the past 12 months and two or three more systems hope to achieve their first successful launch in 2021. There is evidence that this could be the year when the small launch market finally becomes saturated; however, expectations continue to be high and many new entrants hope that there is room for more providers. -
Hybrid Rocket Propulsion
CZECH TECHNICAL UNIVERSITY IN PRAGUE FACULTY OF TRANSPORTATION Department of Air Transport Bc. Tomáš Cáp HYBRID ROCKET PROPULSION Diploma Thesis 2017 1 2 3 4 Acknowledgements I would like to express my sincere thanks to my thesis advisor, doc. Ing. Jakub Hospodka, PhD., for valuable feedback and support during the process of creation of this thesis. Additionally, I am thankful for moral support extended by my family without which the process of writing this thesis would be significantly more difficult. Čestné prohlášení Prohlašuji, že jsem předloženou práci vypracoval samostatně a že jsem uvedl veškeré použité informační zdroje v souladu s Metodickým pokynem o etické přípravě vysokoškolských závěrečných prací. Nemám žádný závažný důvod proti užití tohoto školního díla ve smyslu § 60 Zákona č. 121/2000 Sb., o právu autorském, o právech souvisejících s právem autorským a o změně některých zákonů (autorský zákon). V Praze dne 29. 5. 2017 ……………………………… Tomáš Cáp 5 Abstrakt Autor: Bc. Tomáš Cáp Název práce: Hybrid Rocket Propulsion Škola: České vysoké učení technické v Praze, Fakulta dopravní Rok obhajoby: 2017 Počet stran: 56 Vedoucí práce: doc. Ing. Jakub Hospodka, PhD. Klíčová slova: hybridní raketový motor, raketový pohon, raketové palivo, komerční lety do vesmíru Cílem této diplomové práce je představení hybridního raketového pohonu coby perspektivní technologie, která do budoucna zřejmě výrazně ovlivní směřování kosmonautiky. Součástí práce je stručný popis konvenčních raketových motorů na tuhá a kapalná paliva a základní popis problematiky hybridních raketových motorů. V druhé části práce jsou zmíněny přibližné náklady na provoz těchto systémů a je provedeno srovnání těchto finančních nákladů v poměru k poskytovanému výkonu. V závěru jsou doporučeny oblasti možných využití vhodné pro hybridní raketové motory vzhledem k současnému stupni jejich technologické vyspělosti.