US Commercial Space Transportation Developments and Concepts

Total Page:16

File Type:pdf, Size:1020Kb

US Commercial Space Transportation Developments and Concepts Federal Aviation Administration 2008 U.S. Commercial Space Transportation Developments and Concepts: Vehicles, Technologies, and Spaceports January 2008 HQ-08368.INDD 2008 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 encourage, 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://www.faa.gov/about/office_org/headquarters_offices/ast/. Federal Aviation Administration Office of Commercial Space Transportation i About FAA/AST 2008 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 2008 U.S. Commercial Space Transportation Developments and Concepts Contents Table of Contents Introduction . .1 Space Competitions . .1 Expendable Launch Vehicle Industry . .2 Reusable Launch Vehicle Industry . .2 Reentry Vehicles and In-Space Technologies . .2 Enabling Technologies . .3 Spaceports . .3 Regulatory Developments . .3 Significant 2007 Events . .4 Space Competitions . .6 Google Lunar X PRIZE . .6 X PRIZE Cup . .6 America’s Space Prize . .7 Centennial Challenges . .7 Expendable Launch Vehicles . .9 Current Expendable Launch Vehicle Systems . .9 Atlas V – United Launch Alliance . .9 Delta II – United Launch Alliance . .9 Delta IV – United Launch Alliance . .10 Minotaur I – Orbital Sciences Corporation . .11 Pegasus XL – Orbital Sciences Corporation . .11 Taurus – Orbital Sciences Corporation . .11 Zenit-3SL – Sea Launch Company, LLC . .11 ELV Development Efforts . .12 ALV – Alliant Techsystems . .12 Aquarius – Space Systems/Loral . .12 Eagle S-series – E’Prime Aerospace Corporation . .13 FALCON SLV – Lockheed Martin Michoud Operations . .14 Nanosat Launch Vehicle – Garvey Spacecraft Corporation . .14 Sprite SLV – Microcosm, Inc. .15 Minotaur IV and V.– Orbital Sciences Corporation . .15 QuickReach – AirLaunch LLC . .16 Taurus 2 – Orbital Sciences Corporation . .16 Z-1 – Zig Aerospace, LLC . .16 Zenit-3SLB – Sea Launch Company, LLC, and Space International Services . .17 NASA Exploration Launch Vehicles . .17 Ares I . .17 Ares V . .18 Sounding Rockets . .18 Black Brant – Bristol Aerospace Limited . .18 Oriole – DTI Associates . .18 Terrier-Orion – DTI Associates . .19 Hybrid Sounding Rocket Program – Lockheed Martin-Michoud . .19 Hybrid Test Rocket – Lockheed Martin-Michoud and Nammo AS . .19 SpaceLoft XL – UP Aerospace . .20 Reusable Launch Vehicles . .21 Commercial RLV Development Efforts . .21 Tiger & Cardinal – Acuity Technologies . .21 MOD – Armadillo Aerospace . .21 Federal Aviation Administration Office of Commercial Space Transportation iii Contents 2008 U.S. Commercial Space Transportation Developments and Concepts BSC Spaceship – Benson Space Company . .22 New Shepard – Blue Origin . .22 Sea Star – Interorbital Systems . .23 Neptune – Interorbital Systems . .23 XA 1.0 – Masten Space Systems . .24 Crusader LL – Micro-Space . .24 Crusader HTS – Micro-Space . .24 Volkon – Paragon Labs . .25 Silver Dart – PlanetSpace . .25 Rocketplane XP – Rocketplane Global . ..
Recommended publications
  • Ares I Upper Stage Powering the Second Phase of a Rocket’S Journey to Space
    National Aeronautics and Space Administration NASA’s Ares I Upper Stage Powering the Second Phase of a Rocket’s Journey to Space Going to the moon and beyond will be a stunning Shortly after J-2X engine cutoff, the Orion cap- achievement and an enduring legacy to future sule will separate from the upper stage. Orion’s generations. Supporting the agency’s mission engine then will ignite to insert the capsule into to explore, learn and progress is NASA’s Ares I low-Earth orbit. The Ares I upper stage – dor- crew launch vehicle, an in-line, two-stage rocket. mant after safe shut-down of the J-2X upper The flagship of the Constellation Program’s space stage engine – will re-enter Earth’s atmosphere facts transportation system, the Ares I will carry the and splash down in the Indian Ocean. The upper Orion spacecraft and its crew on missions to the stage and J-2X engine will not be reused. International Space Station and then later on to the moon and beyond. Upper Stage Components The entire Ares I vehicle will be 325 feet tall, with Taking the Ares I on the second phase of its jour- a liftoff mass of 2.0 million pounds and payload ney from Earth will be the spacecraft’s second, capacity of 56,200 pounds mass to low Earth or upper, stage, powered by the J-2X engine. orbit for International Space Station missions, Approximately 133 seconds after liftoff, the Ares and 55,600 pounds mass for lunar missions. I upper stage will separate from the vehicle’s first A self-supporting cylindrical structure, the Ares stage, and the J-2X will ignite.
    [Show full text]
  • Voronezh Tyre Plant Company Profile Company Name (Short): Vshz CJSC CEO: Valeriy Y
    Dear readers, The industrial policy pursued by the regional government is in close alignment with the Devel- opment Strategy of Voronezh region up to 2020. It has been approved after thorough consideration and negotiations with non-governmental organi- zations and professional experts. Thus, the region is in for radical system changes in the regional economy. The regional government is successfully develop- ing innovative system. The main directions of clus- ter development policy have been outlined, which increases the region’s competitive advantages and enhances connections between branches and in- dustries. The regional government has managed to create congenial investment climate in the region. The government is coming up with new ways of supporting Rus- sian and foreign investors, developing the system of subsidies and preferences. Innovative industrial parks and zones are set up. Their infrastructure is financed from the state and regional budgets. Voronezh region is one of top 10 in the investment attractiveness rating and is carrying out over 30 investment projects. All the projects are connected with technical re-equipment of companies and creation of high-technology manufac- turers. The number of Russian and foreign investors is constantly increasing. In the Catalogue of Industrial Companies of Voronezh Region, you will find in- formation on the development of industries in Voronezh region, structural and quality changes in the industrial system. Having read this catalogue, you will learn about the industrial potential of Vo- ronezh region, the companies’ production facilities, history and product range. The regional strategy is based on coordinated efforts, a constructive dialogue between private businesses, the government and non-governmental organiza- tions.
    [Show full text]
  • Organización Latinoamericana De Energía Latin American Energy Orga,Nization
    Marzo - Abril/82 March - April/82 Organización Latinoamericana de Energía Latin American Energy Orga,nization LOS PRECIOS DE LA ENERGJA: INSTRUMENTO DE POLITICA Y PLANIFl- CACION ENERGETICA ENERGY PRICING: A TOOL FOR ENERGY PLANNING ANO POLICY - MAKlNG ENERGIA Y EVALUACION o/ DEL IMPACTO AMBIENTAL ENERGY ANO Tl~E EVALUATION OF ITS ENVIRONMENTAL IMPACT COLOMBIA: ANTE LA NUEVA ERA DEL CARBON COLOMBIA: ON THE BRINK OF A NEW COAL ERA L.-. .....------------------------------------ ... Organización Latinoamericana de Energía lada ORGANO DE D!VULGACION TECNICA DE LA ORGAN!ZAC!ON LATINOAMERICANA · DE ENERGIA (OLAOE) PERIODICAL FOR DISSEMINATION MARZO,.. APR!L/82 OF THE LATIN AMERICAN ENERGY ORGANIZATION MARCH ~ APRIL/82 EDITORIAL 3- 11 EDITORIAL 2 6 LOS PRECIOS DE LA ENERGIA: INSTRUMENTO DE POLITICA Y PLANIFl­ CAG/ON ENERGETICA 5-10 ibb, dJ.(:H~í'.:'i · ENERGY PRICING: A TOOL FOR ENERGY PLANNING ANO POLICY ­ MAKING o~c.r~. ¡~· 1.1- \~ 1 '\l; \lE.~.~ET{Gy ANO THE EVALUATION OF ITS . ENVIRONMENTAL IMPACT \-\::¡' ".) 1. <:~'<!.'.l..~~~; , C:\..i·,~'t >\ •.3 COLOvMBIA: ANTE LA NUEVA ERA DEL. \ · CARBON '. 19- r C) ll. \' L._ +o\~ . COLOMBIA: ON THE BRINK OF A NEW GOAL ERA Los artículos firmados san de la exclusiva responsabilidad de sus autores y no expresan, necesariamente. la posición oficial de la Secre- taria Permanente. Toda colaboración deberá ser dirigido a la Coordinacion de RR.PP.; Información y Difusión de OLADE: Casina 6413 C. C. l .. Quito, Ecuador. The signed articles are me exclusive responsability of their autnors. and 1hey do not necessarily express the otticia! posrtion 01 the Permanent Secretaria t. Any remarks snould IJe di meted to the Ollice of Orfíusion.
    [Show full text]
  • Human Issues Related to Spacecraft Vibration During Ascent
    Human Issues related to Spacecraft Vibration during Ascent Consultant Report to the Constellation Program Standing Review Board Jonathan B. Clark M.D., M.P.H. Suite NA 425 One Baylor Plaza Baylor College of Medicine Houston TX 77030-3498 1731 Sunset Blvd Houston TX 77005 713 859 1381 281 989 8721 [email protected] [email protected] Opinions expressed herein are those of the author and do not reflect the views of the National Space Biomedical Research Institute (NSBRI), Baylor College of Medicine (BCM), the University of Texas Medical Branch (UTMB), or the National Aeronautics and Space Administration (NASA). Human Issues related to Spacecraft Vibration during Ascent Consultant Report to the Constellation Program Standing Review Board Jonathan B. Clark M.D., M.P.H. Opinions expressed herein are those of the author and do not reflect the views of the National Space Biomedical Research Institute (NSBRI), Baylor College of Medicine (BCM), the University of Texas Medical Branch (UTMB), or the National Aeronautics and Space Administration (NASA). Pogo in Liquid Fueled Rocket Motors The pogo phenomenon, or fuel pump inlet pressure fluctuation/ cavitation due to tuning feed line resonant frequencies was a major concern in the early space program. Pump tests showed that as inlet pressures were reduced toward cavitation, the pump started acting as an amplifier, causing large oscillations in the thrust chamber pressure. As the rocket engine thrust develops, liquid propellant is cyclically forced into the turbopump. This fluctuating fluid pressure is converted into an unintended and variable increase in engine thrust, with the net effect being longitudinal axis vibration that could result in spacecraft structural failure.
    [Show full text]
  • 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 .
    [Show full text]
  • An Assessment of Aerocapture and Applications to Future Missions
    Post-Exit Atmospheric Flight Cruise Approach An Assessment of Aerocapture and Applications to Future Missions February 13, 2016 National Aeronautics and Space Administration An Assessment of Aerocapture Jet Propulsion Laboratory California Institute of Technology Pasadena, California and Applications to Future Missions Jet Propulsion Laboratory, California Institute of Technology for Planetary Science Division Science Mission Directorate NASA Work Performed under the Planetary Science Program Support Task ©2016. All rights reserved. D-97058 February 13, 2016 Authors Thomas R. Spilker, Independent Consultant Mark Hofstadter Chester S. Borden, JPL/Caltech Jessie M. Kawata Mark Adler, JPL/Caltech Damon Landau Michelle M. Munk, LaRC Daniel T. Lyons Richard W. Powell, LaRC Kim R. Reh Robert D. Braun, GIT Randii R. Wessen Patricia M. Beauchamp, JPL/Caltech NASA Ames Research Center James A. Cutts, JPL/Caltech Parul Agrawal Paul F. Wercinski, ARC Helen H. Hwang and the A-Team Paul F. Wercinski NASA Langley Research Center F. McNeil Cheatwood A-Team Study Participants Jeffrey A. Herath Jet Propulsion Laboratory, Caltech Michelle M. Munk Mark Adler Richard W. Powell Nitin Arora Johnson Space Center Patricia M. Beauchamp Ronald R. Sostaric Chester S. Borden Independent Consultant James A. Cutts Thomas R. Spilker Gregory L. Davis Georgia Institute of Technology John O. Elliott Prof. Robert D. Braun – External Reviewer Jefferey L. Hall Engineering and Science Directorate JPL D-97058 Foreword Aerocapture has been proposed for several missions over the last couple of decades, and the technologies have matured over time. This study was initiated because the NASA Planetary Science Division (PSD) had not revisited Aerocapture technologies for about a decade and with the upcoming study to send a mission to Uranus/Neptune initiated by the PSD we needed to determine the status of the technologies and assess their readiness for such a mission.
    [Show full text]
  • Up, Up, and Away by James J
    www.astrosociety.org/uitc No. 34 - Spring 1996 © 1996, Astronomical Society of the Pacific, 390 Ashton Avenue, San Francisco, CA 94112. Up, Up, and Away by James J. Secosky, Bloomfield Central School and George Musser, Astronomical Society of the Pacific Want to take a tour of space? Then just flip around the channels on cable TV. Weather Channel forecasts, CNN newscasts, ESPN sportscasts: They all depend on satellites in Earth orbit. Or call your friends on Mauritius, Madagascar, or Maui: A satellite will relay your voice. Worried about the ozone hole over Antarctica or mass graves in Bosnia? Orbital outposts are keeping watch. The challenge these days is finding something that doesn't involve satellites in one way or other. And satellites are just one perk of the Space Age. Farther afield, robotic space probes have examined all the planets except Pluto, leading to a revolution in the Earth sciences -- from studies of plate tectonics to models of global warming -- now that scientists can compare our world to its planetary siblings. Over 300 people from 26 countries have gone into space, including the 24 astronauts who went on or near the Moon. Who knows how many will go in the next hundred years? In short, space travel has become a part of our lives. But what goes on behind the scenes? It turns out that satellites and spaceships depend on some of the most basic concepts of physics. So space travel isn't just fun to think about; it is a firm grounding in many of the principles that govern our world and our universe.
    [Show full text]
  • Atlas Launch System Mission Planner's Guide, Atlas V Addendum
    ATLAS Atlas Launch System Mission Planner’s Guide, Atlas V Addendum FOREWORD This Atlas V Addendum supplements the current version of the Atlas Launch System Mission Plan- ner’s Guide (AMPG) and presents the initial vehicle capabilities for the newly available Atlas V launch system. Atlas V’s multiple vehicle configurations and performance levels can provide the optimum match for a range of customer requirements at the lowest cost. The performance data are presented in sufficient detail for preliminary assessment of the Atlas V vehicle family for your missions. This guide, in combination with the AMPG, includes essential technical and programmatic data for preliminary mission planning and spacecraft design. Interface data are in sufficient detail to assess a first-order compatibility. This guide contains current information on Lockheed Martin’s plans for Atlas V launch services. It is subject to change as Atlas V development progresses, and will be revised peri- odically. Potential users of Atlas V launch service are encouraged to contact the offices listed below to obtain the latest technical and program status information for the Atlas V development. For technical and business development inquiries, contact: COMMERCIAL BUSINESS U.S. GOVERNMENT INQUIRIES BUSINESS INQUIRIES Telephone: (691) 645-6400 Telephone: (303) 977-5250 Fax: (619) 645-6500 Fax: (303) 971-2472 Postal Address: Postal Address: International Launch Services, Inc. Commercial Launch Services, Inc. P.O. Box 124670 P.O. Box 179 San Diego, CA 92112-4670 Denver, CO 80201 Street Address: Street Address: International Launch Services, Inc. Commercial Launch Services, Inc. 101 West Broadway P.O. Box 179 Suite 2000 MS DC1400 San Diego, CA 92101 12999 Deer Creek Canyon Road Littleton, CO 80127-5146 A current version of this document can be found, in electronic form, on the Internet at: http://www.ilslaunch.com ii ATLAS LAUNCH SYSTEM MISSION PLANNER’S GUIDE ATLAS V ADDENDUM (AVMPG) REVISIONS Revision Date Rev No.
    [Show full text]
  • PCEC V2.3 (For Real This Time)
    PCEC v2.3 (For Real This Time) 2021 NASA Cost & Schedule Symposium 14 Apr 2021 Brian Alford Mark Jacobs Booz Allen Hamilton TGS Consultants Shawn Hayes Richard Webb TGS Consultants KAR Enterprises NASA MSFC Victory MIPSSSolutions Team SB Diversity Outline • PCEC Overview • Robotic SC Updates • CASTS Updates • PCEC v2.3 Interface Updates • Closing Victory Solutions MIPSS Team 2 What is PCEC? • The Project Cost Estimating Capability (PCEC) is the primary NASA in-house developed parametric tool for estimating the cost of robotic missions, launch vehicles, crewed vehicles, etc. – Overarching tool for creating an estimate that spans the full NASA WBS – CERs included out-of-the-box for estimating the costs of a flight system (e.g., thermal) and support functions (e.g., project management) – Connects to other NASA-sponsored specialized tools to cover the complete NASA WBS (e.g., NICM, MOCET) – Excel-based (presented as add-in in the Ribbon) with completely visible calculations and code – Consists of the PCEC Interface (the Ribbon and supporting code) and the PCEC Library (the artifacts used to estimate cost) – Available to the General Public Victory Solutions MIPSS Team 3 What is PCEC? Cont’d • PCEC comprises two primary ‘models’, offered seamlessly to the user under a single, integrated tool – Robotic Spacecraft (Robotic SC) – Crewed and Space Transportation Systems (CASTS) • These models have separate data normalizations, collections of CERs, core WBSs, modeling approaches, estimating template worksheets, and scope – Estimating artifacts constitute
    [Show full text]
  • Atlas V Cutaway Poster
    ATLAS V Since 2002, Atlas V rockets have delivered vital national security, science and exploration, and commercial missions for customers across the globe including the U.S. Air Force, the National Reconnaissance Oice and NASA. 225 ft The spacecraft is encapsulated in either a 5-m (17.8-ft) or a 4-m (13.8-ft) diameter payload fairing (PLF). The 4-m-diameter PLF is a bisector (two-piece shell) fairing consisting of aluminum skin/stringer construction with vertical split-line longerons. The Atlas V 400 series oers three payload fairing options: the large (LPF, shown at left), the extended (EPF) and the extra extended (XPF). The 5-m PLF is a sandwich composite structure made with a vented aluminum-honeycomb core and graphite-epoxy face sheets. The bisector (two-piece shell) PLF encapsulates both the Centaur upper stage and the spacecraft, which separates using a debris-free pyrotechnic actuating 200 ft system. Payload clearance and vehicle structural stability are enhanced by the all-aluminum forward load reactor (FLR), which centers the PLF around the Centaur upper stage and shares payload shear loading. The Atlas V 500 series oers 1 three payload fairing options: the short (shown at left), medium 18 and long. 1 1 The Centaur upper stage is 3.1 m (10 ft) in diameter and 12.7 m (41.6 ft) long. Its propellant tanks are constructed of pressure-stabilized, corrosion-resistant stainless steel. Centaur is a liquid hydrogen/liquid oxygen-fueled vehicle. It uses a single RL10 engine producing 99.2 kN (22,300 lbf) of thrust.
    [Show full text]
  • Los Motores Aeroespaciales, A-Z
    Sponsored by L’Aeroteca - BARCELONA ISBN 978-84-608-7523-9 < aeroteca.com > Depósito Legal B 9066-2016 Título: Los Motores Aeroespaciales A-Z. © Parte/Vers: 1/12 Página: 1 Autor: Ricardo Miguel Vidal Edición 2018-V12 = Rev. 01 Los Motores Aeroespaciales, A-Z (The Aerospace En- gines, A-Z) Versión 12 2018 por Ricardo Miguel Vidal * * * -MOTOR: Máquina que transforma en movimiento la energía que recibe. (sea química, eléctrica, vapor...) Sponsored by L’Aeroteca - BARCELONA ISBN 978-84-608-7523-9 Este facsímil es < aeroteca.com > Depósito Legal B 9066-2016 ORIGINAL si la Título: Los Motores Aeroespaciales A-Z. © página anterior tiene Parte/Vers: 1/12 Página: 2 el sello con tinta Autor: Ricardo Miguel Vidal VERDE Edición: 2018-V12 = Rev. 01 Presentación de la edición 2018-V12 (Incluye todas las anteriores versiones y sus Apéndices) La edición 2003 era una publicación en partes que se archiva en Binders por el propio lector (2,3,4 anillas, etc), anchos o estrechos y del color que desease durante el acopio parcial de la edición. Se entregaba por grupos de hojas impresas a una cara (edición 2003), a incluir en los Binders (archivadores). Cada hoja era sustituíble en el futuro si aparecía una nueva misma hoja ampliada o corregida. Este sistema de anillas admitia nuevas páginas con información adicional. Una hoja con adhesivos para portada y lomo identifi caba cada volumen provisional. Las tapas defi nitivas fueron metálicas, y se entregaraban con el 4 º volumen. O con la publicación completa desde el año 2005 en adelante. -Las Publicaciones -parcial y completa- están protegidas legalmente y mediante un sello de tinta especial color VERDE se identifi can los originales.
    [Show full text]
  • Reusable Rocket Upper Stage Development of a Multidisciplinary Design Optimisation Tool to Determine the Feasibility of Upper Stage Reusability L
    Reusable Rocket Upper Stage Development of a Multidisciplinary Design Optimisation Tool to Determine the Feasibility of Upper Stage Reusability L. Pepermans Technische Universiteit Delft Reusable Rocket Upper Stage Development of a Multidisciplinary Design Optimisation Tool to Determine the Feasibility of Upper Stage Reusability by L. Pepermans to obtain the degree of Master of Science at the Delft University of Technology, to be defended publicly on Wednesday October 30, 2019 at 14:30 AM. Student number: 4144538 Project duration: September 1, 2018 – October 30, 2019 Thesis committee: Ir. B.T.C Zandbergen , TU Delft, supervisor Prof. E.K.A Gill, TU Delft Dr.ir. D. Dirkx, TU Delft This thesis is confidential and cannot be made public until October 30, 2019. An electronic version of this thesis is available at http://repository.tudelft.nl/. Cover image: S-IVB upper stage of Skylab 3 mission in orbit [23] Preface Before you lies my thesis to graduate from Delft University of Technology on the feasibility and cost-effectiveness of reusable upper stages. During the accompanying literature study, it was determined that the technology readiness level is sufficiently high for upper stage reusability. However, it was unsure whether a cost-effective system could be build. I have been interested in the field of Entry, Descent, and Landing ever since I joined the Capsule Team of Delft Aerospace Rocket Engineering (DARE). During my time within the team, it split up in the Structures Team and Recovery Team. In September 2016, I became Chief Recovery for the Stratos III student-built sounding rocket. During this time, I realised that there was a lack of fundamental knowledge in aerodynamic decelerators within DARE.
    [Show full text]