Mars Correct: Critique of All Nasa Mars Weather Data
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Venona Special Studies
- 1 - Venona Project Special Studies Transcribed by Students of the Mercyhurst College Institute for Intelligence Studies Arranged by John Earl Haynes, Library of Congress, 2010 COVER NAMES IN NEW YORK TRAFFIC p. 2 UNIDENTIFIED COVER NAMES IN NEW YORK TRAFFIC p. 86 COVER NAMES IN SAN FRANCISCO TRAFFIC p. 92 COVER NAMES IN WASHINGTON TRAFFIC p. 123 ADDITIONAL COVERNAMES AND RELATED INFORMATION IN DIPLOMATIC TRAFFIC p. 127 REVISED TRANSLATION OF MESSAGE ON ANTENNA-LIBERAL'S WIFE ETHEL p. 135 THE COVERNAMES "ANTENNA" AND "LIBERAL" IN . MESSAGES p. 139 ESSAGES IN . INVOLVING THE COVERNAME"ENORMOZ" AND THE NAMES OF NUCLEAR PHYSICISTS, ETC. p. 147 UNDATED REPORT OF MEREDITH GARDNER p. 155 DEVELOPMENT OF THE “G--“HOMER” [“GOMER”] CASE p. 158 THE KOMAR (KRAVCHENKO) AFFAIR IN . MESSAGES p. 161 REVISED TRANSLATION OF TWO . MESSAGES ON CHANGES IN COVERNAMES p. 170 THE COVERNAME "KARAS" IN. TRAFFIC p. 178 THE COVERNAMES "TÉNOR", "BAS", AND "CHETÁ" (? IN . TRAFFIC p. 181 - 2 - Special Study Cover Names in New York Traffic - 3 - cover-name Message number Date Publication reference S/ or 3/NBF/ 19 N.Y. to M. 812 29053 JKI 06 T1022 1B-1910 0027A ABRAM N.Y. to M. 992 24063 JKR 14 T872√ 1B-7518 0005A JACK SOBLE 1086 06073 JKV 48 T873√ 2A-0011 1957 29113 NNNNNN T939√ 625 04054 JHD 48 T916√ 851 15064 JIJ 40 T10.1√ 1146 10084 JHM 41 T123√ 1251 02094 JHN 12 T301√ (to ChEKh) 0005B 1353 23094 JHO 42 T289√ 1449 12104 JIL 37 T106√ 1754 14124 JHZ 49 T6√ 48 11015 JHV 37 (NSA)T1941 AVGUR 2A-0013 1638 (AUGUR) N.Y. -
Industry at the Edge of Space Other Springer-Praxis Books of Related Interest by Erik Seedhouse
IndustryIndustry atat thethe EdgeEdge ofof SpaceSpace ERIK SEEDHOUSE S u b o r b i t a l Industry at the Edge of Space Other Springer-Praxis books of related interest by Erik Seedhouse Tourists in Space: A Practical Guide 2008 ISBN: 978-0-387-74643-2 Lunar Outpost: The Challenges of Establishing a Human Settlement on the Moon 2008 ISBN: 978-0-387-09746-6 Martian Outpost: The Challenges of Establishing a Human Settlement on Mars 2009 ISBN: 978-0-387-98190-1 The New Space Race: China vs. the United States 2009 ISBN: 978-1-4419-0879-7 Prepare for Launch: The Astronaut Training Process 2010 ISBN: 978-1-4419-1349-4 Ocean Outpost: The Future of Humans Living Underwater 2010 ISBN: 978-1-4419-6356-7 Trailblazing Medicine: Sustaining Explorers During Interplanetary Missions 2011 ISBN: 978-1-4419-7828-8 Interplanetary Outpost: The Human and Technological Challenges of Exploring the Outer Planets 2012 ISBN: 978-1-4419-9747-0 Astronauts for Hire: The Emergence of a Commercial Astronaut Corps 2012 ISBN: 978-1-4614-0519-1 Pulling G: Human Responses to High and Low Gravity 2013 ISBN: 978-1-4614-3029-2 SpaceX: Making Commercial Spacefl ight a Reality 2013 ISBN: 978-1-4614-5513-4 E r i k S e e d h o u s e Suborbital Industry at the Edge of Space Dr Erik Seedhouse, M.Med.Sc., Ph.D., FBIS Milton Ontario Canada SPRINGER-PRAXIS BOOKS IN SPACE EXPLORATION ISBN 978-3-319-03484-3 ISBN 978-3-319-03485-0 (eBook) DOI 10.1007/978-3-319-03485-0 Springer Cham Heidelberg New York Dordrecht London Library of Congress Control Number: 2013956603 © Springer International Publishing Switzerland 2014 This work is subject to copyright. -
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. -
Orion Capsule Launch Abort System Analysis
Orion Capsule Launch Abort System Analysis Assignment 2 AE 4802 Spring 2016 – Digital Design and Manufacturing Georgia Institute of Technology Authors: Tyler Scogin Michel Lacerda Jordan Marshall Table of Contents 1. Introduction ......................................................................................................................................... 4 1.1 Mission Profile ............................................................................................................................. 7 1.2 Literature Review ........................................................................................................................ 8 2. Conceptual Design ............................................................................................................................. 13 2.1 Design Process ........................................................................................................................... 13 2.2 Vehicle Performance Characteristics ......................................................................................... 15 2.3 Vehicle/Sub-Component Sizing ................................................................................................. 15 3. Vehicle 3D Model in CATIA ................................................................................................................ 22 3.1 3D Modeling Roles and Responsibilities: .................................................................................. 22 3.2 Design Parameters and Relations:............................................................................................ -
Lunar Life Sciences Payload Assessment
Lunar Surface Science Workshop 2020 (LPI Contrib. No. 2241) 5077.pdf LUNAR LIFE SCIENCES PAYLOAD ASSESSMENT. S. C. Sun1, F. Karouia2, M. P. Lera3, M. P. Parra1, H. E. Ray4, A. J. Ricco1, S. M. Spremo1. 1NASA Ames Research Center, 2Blue Marble Space Institute of Science, 3KBR, 4ASRC Federal Space and Defense, Inc. Introduction: The Moon provides a unique site to ISS, including systems that integrate into EXPRESS study living organisms. The fractional gravity and (EXpedite the PRocessing of ExperimentS for Space) unique radiation environment have similarities to Mars Racks or are external space exposure research facilities. and will help us understand how life will respond to These same systems can be the basis for future payload conditions on the red planet. Martian and lunar envi- systems for experiments to be performed beyond Low ronments can be simulated on the ground but not to high Earth Orbit. Such facilities would need to be adapted to fidelity. Altered gravity and increased radiation are dif- be compatible with the new research platforms and ficult to replicate simultaneously, which makes study- function in the harsher radiation environment found out- ing their combined effect difficult. The International side the magnetosphere. If Gateway and a lunar based- Space Station, and previously, the Space Shuttle, pro- lab could provide EXPRESS-compatible interfaces, lev- vided a microgravity environment, and could simulate eraging hardware developed for ISS would be more fea- fractional-g only via an onboard centrifuge. Because sible. the ISS and Space Shuttle orbits were within the Earth’s Gaps in Capabilities: Many of the payload systems magnetosphere, experiments on those platforms have that have been developed require human tending. -
19700031865.Pdf
1. Report No. 2. Government Accession No. 3. Recipient's Catalog No. NASA TM X-2075 4. Title and Subtitle 5. Report Date EFFECTOFRETROROCKETCANTANGLEON October 1970 6. Performing Organization Code GROUND EROSION - A SCALED VIKING STUDY 7. Author(s) 8. Performing Organization Report No. Leonard V. Clark L-7376 IO. Work Unit No. 9. Performing Organization Name and Address 124-08-29-01 NASA Langley Research Center 11. Contract or Grant No. Hampton, Va. 23365 13. Type of Report and Period Covered 12. Sponsoring Agency Name and Address Technical Memorandum National Aeronautics and Space Administration 14. Sponsoring Agency Code Washington, D.C. 20546 ~ 16. Abstract An experimental study was conducted at the Langley Research Center to evaluate the relative merits of canting the Viking lander retrorockets toward the spacecraft center line as a means of reducing rocket-exhaust disturbance of the surface of Mars. This paper describes the experimental study, outlines the scaling scheme of the tests, and briefly dis- cusses significant data trends. The results of this exploratory study indicate that canting of the retrorockets toward the center of the spacecraft does reduce ground erosion of the landing site from that produced by a lander configuration with downward-directed retro- rockets. Obviously, before canting the Viking lander retrorockets, it would be necessary to weigh this reduction in surface disturbance against the attendant loss of thrust due to canting. 17. Key Words (Suggested by Author(s) ) 18. Distribution Statement Jet impingement Unclassified - Unlimited Rocket-exhaust effects 19. Security Classif. (of this report) 20. Security Classif. (of this page) 21. No. -
18Th EANA Conference European Astrobiology Network Association
18th EANA Conference European Astrobiology Network Association Abstract book 24-28 September 2018 Freie Universität Berlin, Germany Sponsors: Detectability of biosignatures in martian sedimentary systems A. H. Stevens1, A. McDonald2, and C. S. Cockell1 (1) UK Centre for Astrobiology, University of Edinburgh, UK ([email protected]) (2) Bioimaging Facility, School of Engineering, University of Edinburgh, UK Presentation: Tuesday 12:45-13:00 Session: Traces of life, biosignatures, life detection Abstract: Some of the most promising potential sampling sites for astrobiology are the numerous sedimentary areas on Mars such as those explored by MSL. As sedimentary systems have a high relative likelihood to have been habitable in the past and are known on Earth to preserve biosignatures well, the remains of martian sedimentary systems are an attractive target for exploration, for example by sample return caching rovers [1]. To learn how best to look for evidence of life in these environments, we must carefully understand their context. While recent measurements have raised the upper limit for organic carbon measured in martian sediments [2], our exploration to date shows no evidence for a terrestrial-like biosphere on Mars. We used an analogue of a martian mudstone (Y-Mars[3]) to investigate how best to look for biosignatures in martian sedimentary environments. The mudstone was inoculated with a relevant microbial community and cultured over several months under martian conditions to select for the most Mars-relevant microbes. We sequenced the microbial community over a number of transfers to try and understand what types microbes might be expected to exist in these environments and assess whether they might leave behind any specific biosignatures. -
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. -
Reusable Stage Concepts Design Tool
DOI: 10.13009/EUCASS2019-421 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) DOI: ADD DOINUMBER HERE Reusable stage concepts design tool Lars Pepermans?, Barry Zandbergeny ?Delft University of Technology Kluyverweg 1, 2629 HS Delft [email protected] yDelft University of Technology Kluyverweg 1, 2629 HS Delft Abstract Reusable launch vehicles hold the promise of substantially reducing the cost of access to space. Many different approaches towards realising a reusable rocket exist or are being proposed. This work focuses on the use of an optimisation method for conceptual design of non-winged reusable upper stages, thereby allowing it to take into account landing on land, sea or mid-air retrieval as well as landing the full stage or the engine only. As the optimisation criterion, the ratio of the specific launch cost of the reusable to the expendable version is used. The tool also provides for a Monte Carlo analysis, which allows for investigating the ruggedness of the design solution(s) found. The article will describe the methods implemented in the Conceptual Reusability Design Tool (CRDT) together with the modifications made to ParSim v3, a simulation tool by Delft Aerospace Rocket Engi- neering. Furthermore, it will present the steps taken to verify and validate CRDT. Finally, several example cases are presented based on the Atlas V-Centaur launch vehicle. The cases demonstrate the tools capa- bility of finding optimum and the sensitivity of the found optimum. However, it also shows the optimum when the user disables some Entry Descent and Landing (EDL) options. 1. Introduction To make space more accessible, one can reduce the cost of an orbital launch. -
NASA Ames to Establish Nationwide Lunar Science Institute
November 2007 Worden gives upbeat message about future work for Ames BY JOHN BLUCK "We have switched material to In an upbeat talk to a crowd that phenolic impregnated carbon abla- filled the Ames main auditorium, tor (PICA), a (heat shield) material Ames Center Director S. Pete Worden developed here," Worden noted. His outlined an exciting future at Ames projected slide also listed Ames as that includes new work in exploration, leading PICA development and test- science and aeronautics -- each about a ing both for the Crew Exploration Ve- third of the center's efforts, he said. "I hicle, now called Orion, and the Mars have a gazillion charts to go through," Science Laboratory (MSL), which has photo by Eric James NASA he said. a planned launch date in fall 2009. His wide-ranging presentation Worden said that Ames' arc jets about Ames touched on moon explo- facility "a unique facility in the world." ration, a lunar institute, moon dust re- He added, "We want to upgrade search, heat shield work for spacecraft them." destined for the moon and Mars, a Mars sample "cache box" assignment, Life Sciences rising supercomputer capability, small "We are getting additional life Ames Center Director S. Pete Worden responds satellite work with a potential for support tasks assigned by Johnson to a question during the recent upbeat talk he many missions, increased astrobiology (and Marshall)," Worden said. "This is gave to the center about the future of Ames. work, growing cooperation among significant." continued on page 5 academia, and commercial partners and Ames and much more. -
6 FOTON RETRIEVABLE CAPSULES This Section Is Aimed at Providing New and Experienced Users with Basic Utilisation Information Regarding Foton Retrievable Capsules
6 FOTON RETRIEVABLE CAPSULES This section is aimed at providing new and experienced users with basic utilisation information regarding Foton retrievable capsules. It begins with an introduction to the Foton capsule. 6.1 Introduction to Foton Capsules 6.1.1 What Are Foton Capsules? Foton capsules (Figure 6-1 and Figure 6-2) are unmanned, retrievable capsules, derived from the design of the 1960’s Soviet Vostok manned spacecraft and the Zenit military reconnaissance satellite. These capsules are very similar to the Bion and Resurs-F satellites introduced by the Soviets in the 1970’s, for biological research and Earth natural resources investigation, respectively. The first Foton capsule was launched in 1985 as Cosmos 1645 and only with the fourth launch in 1988 was the spacecraft officially designated Foton (Foton-4). These capsules are launched into near-circular, low-earth orbits by a Soyuz-U rocket, providing researchers with gravity levels less than 10 -5 g, for missions lasting approximately 2 weeks. The earlier Foton missions were conceived primarily for materials science research, but later missions also began to include experiments in the fields of fluid physics, biology and radiation dosimetry. ESA’s participation in the Foton programme began in 1991 with a protein crystallisation experiment on-board Foton-7, followed by a further 35 experiments up to and including the Foton- 12 mission in 1999. In 2002, ESA provided a large number of experiments for the Foton-M1 mission (the first flight of an upgraded version of the Foton spacecraft). This mission ended in disaster when the Soyuz launcher rocket exploded shortly after lift-off due to a malfunction in one of its engines. -
Genesat (Launched Dec 2006), – Pre-Sat/Nanosail-D (Aug 2008) – Pharmasat (Launched May 2009), – O/OREOS (Planned May
National Aeronautics and Space Administration Free Flyer Utilization for Biology Research John W. Hines Chief Technologist, Engineering Directorate Technical Director, Nanosatellite Missions NASA-Ames Research Center NASA Applications of BioScience/BioTechnology HumanHuman ExplorationExploration EmphasisEmphasis FundamentalFundamental ExploratiExploratioonn Subsystems BiologyBiology Subsystems EmphasisEmphasis HumansHumans SmallSmall OrganismsOrganisms (Mice,(Mice, Rats) Rats) TiTissussue,e, O Orrgansgans MammalianMammalian CellsCells Human Health Emphasis ModelModel Organisms, BioMolecules Organisms, BioMolecules MicrobesMicrobes 2 4 Free-Flyer Utilization Free Flyer Features • Advantage: Relatively inexpensive means to increase number of flight opportunities • Capabilities: – Returnable capsule to small secondary non-recoverable satellites, and/or – In-situ measurement and control with autonomous sample management • Command and Control: Fully automated or uplinked command driven investigations. • Research data: Downlink and/or receipt of the samples • Collaborations: Interagency, academic, commercial and international Russian Free Flyers Early Free Flyers NASA Biosatellite I, II, 1966-67 NASA Biosatellite III, 1969 Nominal 3d flights Nominal 20d flight • Response to microgravity & • Spaceflight responses of non-human radiation: various biological species primates • Onboard radiation source Timeline of Russian-NASA Biology Spaceflights Collaborations Bion* Characteristics Bion Rationale • Increases access to space • Proven Platforms