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Concept Study of a Cislunar Outpost Architecture and Associated Elements That Enable a Path to Mars
Concept Study of a Cislunar Outpost Architecture and Associated Elements that Enable a Path to Mars Presented by: Timothy Cichan Lockheed Martin Space [email protected] Mike Drever Lockheed Martin Space [email protected] Franco Fenoglio Thales Alenia Space Italy [email protected] Willian D. Pratt Lockheed Martin Space [email protected] Josh Hopkins Lockheed Martin Space [email protected] September 2016 © 2014 Lockheed Martin Corporation Abstract During the course of human space exploration, astronauts have travelled all the way to the Moon on short flights and have logged missions of a year or more of continuous time on board Mir and the International Space Station (ISS), close to Earth. However, if the long term goal of space exploration is to land humans on the surface of Mars, NASA needs precursor missions that combine operating for very long durations and great distances. This will allow astronauts to learn how to work in deep space for months at a time and address many of the risks associated with a Mars mission lasting over 1,000 days in deep space, such as the inability to abort home or resupply in an emergency. A facility placed in an orbit in the vicinity of the Moon, called a Deep Space Transit Habitat (DSTH), is an ideal place to gain experience operating in deep space. This next generation of in-space habitation will be evolvable, flexible, and modular. It will allow astronauts to demonstrate they can operate for months at a time beyond Low Earth Orbit (LEO). The DSTH can also be an international collaboration, with partnering nations contributing elements and major subsystems, based on their expertise. -
Jenkins 2000 AIRLOCK & CONNECTIVE TUNNEL DESIGN
Jenkins_2000 AIRLOCK & CONNECTIVE TUNNEL DESIGN AND AIR MAINTENANCE STRATEGIES FOR MARS HABITAT AND EARTH ANALOG SITES Jessica Jenkins* ABSTRACT For a manned mission to Mars, there are numerous systems that must be designed for humans to live safely with all of their basic needs met at all times. Among the most important aspects will be the retention of suitable pressure and breathable air to sustain life. Also, due to the corrosive nature of the Martian dust, highly advanced airlock systems including airshowers and HEPA filters must be in place so that the interior of the habitat and necessary equipment is protected from any significant damage. There are multiple current airlocks that are used in different situations, which could be modified for use on Mars. The same is true of connecting tunnels to link different habitat modules. In our proposed Mars Analog Challenge, many of the airlock designs and procedures could be tested under simulated conditions to obtain further information without actually putting people at risk. Other benefits of a long-term study would be to test how the procedures affect air maintenance and whether they need to be modified prior to their implementation on Mars. INTRODUCTION One of the most important factors in the Mars Habitat design involves maintaining the air pressure within the habitat. Preservation of breathable air will be an extremely vital part of the mission, as very little can be found in situ. Since Mars surface expeditions will be of such long duration, it is imperative that the airlock designs incorporate innovative air maintenance strategies. For our proposed Earth Analog Site competition, many of the components of these designs can be tested, as can the procedures required for long-duration habitation on Mars. -
Spacesuits Have Been Created, but We Want to Go Further
Science and Innovation A Boeing/Teaching Channel Partnership EXTREME BIOSUITS Student Handbook Science and Innovation Extreme Biosuits Student Handbook Engineering Design Process Step 1 Identify the Need or Problem Describe the engineering design challenge to be solved. Include the limits and constraints, customer description, and an explanation of why solving this challenge is important. Step 2 Research Criteria and Constraints Research how others have solved this or similar problems, and discover what materials have been used. Be sure to thoroughly research the limitations and design requirements for success. Step 3 Brainstorm Possible Solutions Use your knowledge and creativity to generate as many solutions as possible. During this brainstorming stage, do not reject any ideas. Step 4 Select the Best Solution Each team member presents their solution ideas to the team. Team members annotate how each solution does or does not meet each design requirement. The team then agrees on a solution, or combination of solutions, that best meets the design requirements. Step 5 Construct a Prototype Develop an operating version of the solution. Step 6 Test Test your solution. Annotate the results from each test to share with your team. Step 7 Present Results Present the results from each test to the team. Step 8 Redesign Determine a redesign to address failure points and/or design improvements. The design process involves multiple iterations and redesigns. Redesign is based on the data from your tests, your team discussions as to the next steps to improve the design, and the engineering design process Steps 1 through 7. Once your team is confident of a prototype solution, you present the results to the client. -
Mark V Diving Helmet
Historical Diver, Number 5, 1995 Item Type monograph Publisher Historical Diving Society U.S.A. Download date 06/10/2021 19:38:35 Link to Item http://hdl.handle.net/1834/30848 IDSTORI DIVER The Offical Publication of the Historical Diving Society U.S.A. Number 5 Summer 1995 "Constant and incessant jerking and pulling on the signal line or pipe, by the Diver, signifies that he must be instantly pulled up .... " THE WORLDS FIRST DIVING MANUAL Messrs. C.A. and John Deane 1836 "c:lf[{[J a:tk o{ eadz. u.adn l;t thi:1- don't di£ wllfzoul fz.a1Jin5 Co't'towe.J, dofen, pwu!.hau:d O'l made a hefmd a{ :toorh, to gfimju.e (o'r. !JOU'tul{ thl:1 new wo'l.fJ''. 'Wifl'iam 'Bube, "'Beneath 'J,opic dlw;" 1928 HISTORICAL DIVING SOCIETY HISTORICAL DIVER MAGAZINE USA The official publication of the HDSUSA A PUBLIC BENEFIT NON-PROFIT CORPORATION HISTORICAL DIVER is published three times a year C/0 2022 CLIFF DRIVE #119 by the Historical Diving Society USA, a Non-Profit SANTA BARBARA, CALIFORNIA 93109 U.S.A. Corporation, C/0 2022 Cliff Drive #119 Santa Barbara, (805) 963-6610 California 93109 USA. Copyright© 1995 all rights re FAX (805) 962-3810 served Historical Diving Society USA Tel. (805) 963- e-mail HDSUSA@ AOL.COM 6610 Fax (805) 962-3810 EDITORS: Leslie Leaney and Andy Lentz. Advisory Board HISTORICAL DIVER is compiled by Lisa Glen Ryan, Art Bachrach, Ph.D. J. Thomas Millington, M.D. Leslie Leaney, and Andy Lentz. -
Multi Duty (MD) Airlock
Multi Duty (MD) Airlock ■ Versatile airlock can be connected to many different types of storage and conveying devices ■ Square flanged inlet and outlet ■ Highly reliable, rugged design delivers low maintenance service ■ Sealed bearings require no lubrication and provide years of service ■ Available in a wide range of sizes ■ Special options extend service life in challenging applications Application Outboard press fit bearings provide better protection, resulting With tens of thousands of installations throughout the world, the in longer service life. Special wear resistant MD designs are Schenck Process MD airlock is a highly universal airlock used designed to be placed in abrasive environments. Field tests of to meter dry bulk materials under feeding devices, such as bins, these designs show a lifespan up to eight times longer than a hoppers, mixers, screw conveyors and sifters. standard MD airlock. Providing rugged service, the MD is suitable for use in dilute Operating Principle phase vacuum, pressure or combination vacuum/pressure The airlock reliably meters products into conveying lines or pneumatic conveying systems. Low mounting height is ideal storage areas. With open end rotors, the product comes in for space restricted applications. With a low profile and a wide contact with the endplates of the housing. With closed end flange width, the MD airlock is able to match drill hole patterns rotors, the product is confined within the pockets of the rotor. of many competitor’s valves for easy replacement. Features Equipment Rated up to 15 psi pressure differential The MD has a cast housing and endplates with a square flange. Standard temperature rating is 200 ºF (93 °C) The rotor and housing are precision machined to obtain a high Optional high-temperature rated to 450 ºF (232 °C) degree of accuracy and close tolerances. -
Next Term's Project ENAE 483/788D
Discussion of Next Term • Final design project information • Discussion of final exam • Discussion of grading for group projects • Other useful information © 2013 David L. Akin - All rights reserved http://spacecraft.ssl.umd.edu U N I V E R S I T Y O F Next Term’s Project ENAE 483/788D - Principles of Space Systems Design MARYLAND 1 Notes • Due date for project 5 postponed to time of final exam Monday 12/16 • Slides for Tuesday’s class (Sensors and Actuators) posted to Piazza site • Reminders: – Final exam limited single 8.5”x11” sheet of notes – Bring a calculator – Given honest attempt, final will only be counted if it improves overall grade U N I V E R S I T Y O F Next Term’s Project ENAE 483/788D - Principles of Space Systems Design MARYLAND 2 ENAE 483/788D Final Exam Questions • Orbital mechanics • Rocket performance • Reliability • Life support • Power systems • Structural design • Thermal analysis • Cost analysis • Propulsion systems • Systems engineering U N I V E R S I T Y O F Next Term’s Project ENAE 483/788D - Principles of Space Systems Design MARYLAND 3 Grading Rubrik for Group Projects • 10 - essentially perfect • 9 - excellent • 8 - very good • 7 - good • 6 - okay • 5 - minor deficiencies • 4 - significant deficiencies • 3 or below - major deficiencies U N I V E R S I T Y O F Next Term’s Project ENAE 483/788D - Principles of Space Systems Design MARYLAND 4 Fall Term Project Organization Systems Crew Systems Power, Propulsion, and Loads, Structures, and Avionics and Engineering Thermal Mechanisms Software A1 B1 C1 D1 E1 A2 -
ATMOSPHERIC DIVING SUITS Kyznecov RR, Egorov IB
УДК 004.9 ATMOSPHERIC DIVING SUITS Kyznecov R.R., Egorov I.B., Scientific adviser: senior teacher Labusheva T.M. Siberian Federal University In our lives, information technology is found almost in everything - in smart stoves and in supercomputers. And atmospheric diving suits are not an exception. The report is dedicated to them. It will show the way they are connected to our future profession and what they can do. The most important periods of the atmospheric diving suit evolution are given below: LETHBRIDGE 1715 (UK) The first recorded attempt at protecting a diver in a rigid armor was done by John Lethbridge of Devonshire. It happened in England in 1715. The oak suit offered by him had a viewing port and holes for the diver’s arms. Water was kept out of the suit by greased leather cuffs which sealed around the operator’s arms. The device was said to have made many working dives to 60ft/18m. Lethbridge’s device probably performed as claimed. It is known from the painstaking work of Belgian expert, Robert Stenuit. Working under the protection of Comex with assistance from Comex’s founder, Henri Delauze, Stenuit imitated and operated as the "Lethbridge Engine," using only materials and techniques available in day time. JIM In 1960s an English company called DHB was interested very mush in Atmospheric Diving Suits. With the help of the government it started to perfect the Peress Tritonia suit from 1930 that it found out by coincidence and luck. After performing some tests with the old suit it became obvious that the joints had to be designed again. -
13.012 Marine Hydrodynamics for Ocean Engineers Fall 2004 Quiz #1 Student Name: ˆ4 10
13.012 Marine Hydrodynamics for Ocean Engineers Fall 2004 Quiz #1 Student name: _____________________________________ This is a closed book examination. You are allowed 1 sheet of 8.5” x 11” paper with notes. For the problems in Section A, fill in the answers where indicated by ____________, or in the provided space. When a list of options is presented ([…],[…],[….] etc), circle all the options (all, none, one or more) that apply. Use the following constants unless otherwise specified: 2 3 -6 2 Gravity: g = 10 m/s water density: ρw = 1000 kg/m kinematic viscosity: νw = 1x10 m /s 3 -6 2 Seawater density: ρw = 1025 kg/m kinematic viscosity: νsw = 1x10 m /s 3 -5 2 Air density: ρa = 1 kg/m kinematic viscosity: νa = 1x10 m /s Assume the fluid is incompressible unless otherwise defined. Give all answers in SI units (kg, m, s). All numerical answers MUST have the proper units attached. Part A (30%): 1) A 1 m3 block of aluminum, specific gravity 2.7, is tethered to a piece of cork, specific gravity 0.24. The volume of cork required to keep the block neutrally buoyant in seawater is _______________ and the volume required in fresh water is _______________. Assume both the aluminum and cork are fully submerged and that the weight of the tether is negligible. h 2) The velocity field V= 4 xyiˆ + 10 y2 ˆj+ C zykˆ is valid for C = _____________. The vorticity in this flow field is ω = ______________. This flow field is [irrotational][rotational]. 3) The two linearized boundary conditions at the free surface for linear progressive free-surface gravity waves are _________________ and __________________. -
Title Description Filename Keywords Media Code Time CD Track Index AIR PRESSURIZED AIR BLAST, SCI FI Air 8005 01 1 Air, Ga
Media Title Description FileName Keywords Time CD Track Index Code Air, Gases & Steam;Space 8005- AIR PRESSURIZED AIR BLAST, SCI FI Air 8005_01_1 :01 8005 1 1 Doors, Hatches & Airlocks 01-01 Air, Gases & Steam;Space 8005- AIR PRESSURIZED AIR BLAST, SCI FI Air 8005_01_2 :01 8005 1 2 Doors, Hatches & Airlocks 01-02 Air, Gases & Steam;Space 8005- AIR PRESSURIZED AIR BLAST, SCI FI Air 8005_02_1 :02 8005 2 1 Doors, Hatches & Airlocks 02-01 Air, Gases & Steam;Space 8005- AIR PRESSURIZED AIR BLAST, SCI FI Air 8005_02_2 :01 8005 2 2 Doors, Hatches & Airlocks 02-02 Air, Gases & Steam;Space 8005- AIR PRESSURIZED AIR BLAST, SCI FI Air 8005_03_1 :01 8005 3 1 Doors, Hatches & Airlocks 03-01 Air, Gases & Steam;Space 8005- AIR PRESSURIZED AIR BLAST, SCI FI Air 8005_03_2 :01 8005 3 2 Doors, Hatches & Airlocks 03-02 Air, Gases & Steam;Space 8005- AIR PRESSURIZED AIR BLAST, SCI FI Air 8005_04_1 :01 8005 4 1 Doors, Hatches & Airlocks 04-01 Air, Gases & Steam;Space 8005- AIR PRESSURIZED AIR BLAST, SCI FI Air 8005_04_2 :01 8005 4 2 Doors, Hatches & Airlocks 04-02 Air, Gases & Steam;Space 8005- AIR PRESSURIZED AIR BLAST, SCI FI Air 8005_05_1 :01 8005 5 1 Doors, Hatches & Airlocks 05-01 Air, Gases & Steam;Space 8005- AIR PRESSURIZED AIR BLAST, SCI FI Air 8005_05_2 :01 8005 5 2 Doors, Hatches & Airlocks 05-02 Air, Gases & Steam;Space 8005- AIR PRESSURIZED AIR BLAST, SCI FI Air 8005_05_3 :04 8005 5 3 Doors, Hatches & Airlocks 05-03 Air, Gases & Steam;Space 8005- AIR PRESSURIZED REVERSE AIR POP, SCI FI Air 8005_06_1 :01 8005 6 1 Doors, Hatches & Airlocks 06-01 -
Human Systems Integration of an Extravehicular Activity Space Suit Augmented Reality Display System
Mississippi State University Scholars Junction Theses and Dissertations Theses and Dissertations 1-1-2018 Human Systems Integration of an Extravehicular Activity Space Suit Augmented Reality Display System Paromita Mitra Follow this and additional works at: https://scholarsjunction.msstate.edu/td Recommended Citation Mitra, Paromita, "Human Systems Integration of an Extravehicular Activity Space Suit Augmented Reality Display System" (2018). Theses and Dissertations. 2517. https://scholarsjunction.msstate.edu/td/2517 This Graduate Thesis - Open Access is brought to you for free and open access by the Theses and Dissertations at Scholars Junction. It has been accepted for inclusion in Theses and Dissertations by an authorized administrator of Scholars Junction. For more information, please contact [email protected]. Template C v3.0 (beta): Created by J. Nail 06/2015 Human systems integration of an extravehicular activity space suit augmented reality display system By TITLE PAGE Paromita Mitra A Thesis Submitted to the Faculty of Mississippi State University in Partial Fulfillment of the Requirements for the Degree of Master of Science in Aerospace Engineering. in the Department of Aerospace Engineering. Mississippi State, Mississippi August 2018 Copyright by COPYRIGHT PAGE Paromita Mitra 2018 Human systems integration of an extravehicular activity space suit augmented reality display system By APPROVAL PAGE Paromita Mitra Approved: ____________________________________ Keith Koenig (Major Professor) ____________________________________ -
GNM Silent Killers.Qxd:Layout 1
“A truly engrossing chronicle.” Clive Cussler JAMES P. DELGADO SILENT KILLERS SUBMARINES AND UNDERWATER WARFARE FOREWORD BY CLIVE CUSSLER © Osprey Publishing • www.ospreypublishing.com © Osprey Publishing • www.ospreypublishing.com SUBMARINES AND UNDERWATER WARFARE JAMES P. DELGADO With a foreword by Clive Cussler © Osprey Publishing • www.ospreypublishing.com CONTENTS Foreword 6 Author’s Note 7 Introduction: Into the Deep 11 Chapter 1 Beginnings 19 Chapter 2 “Sub Marine Explorers”: Would-be Warriors 31 Chapter 3 Uncivil Warriors 45 Chapter 4 Missing Links 61 Chapter 5 Later 19th Century Submarines 73 Chapter 6 Transition to a New Century 91 Chapter 7 Early 20th Century Submariness 107 Chapter 8 World War I 123 Chapter 9 Submarines Between the Wars 143 Chapter 10 World War II: the Success of the Submarine 161 Chapter 11 Postwar Innovations: the Rise of Atomic Power 189 Chapter 12 The Ultimate Deterrent: the Role of the 207 Submarine in the Modern Era Chapter 13 Memorializing the Submarine 219 Notes 239 Sources & Select Bibliography 248 Index 260 © Osprey Publishing • www.ospreypublishing.com FOREWORD rom the beginning of recorded history the inhabitants of the earth have had a Fgreat fascination with what exists under the waters of lakes, rivers, and the vast seas. They also have maintained a great fear of the unknown and very few wished to actually go under the surface. In the not too distant past, they had a morbid fear and were deeply frightened of what they might find. Only three out of one hundred old-time sailors could swim because they had no love of water. -
Some Comments on the TA06 Roadmap Relevant to EVA Technology
Some Comments on the TA06 Roadmap Relevant to EVA Technology Edward Hodgson Hamilton Sundstrand Corporation Overview • There is a lot to like – Many promising technology directions with game changing potential – The broad vision of component subsystem development leading to ground integration and validation testing ultimately on ISS is sound. • EVA system may be too narrowly viewed • Some areas need more definition • A few possible gaps are noted • The elephant in the room EVA System May be too Narrowly Viewe d • Includes not only PGA , PLSS , PAS as noted. • Airlock & servicing systems, Tools, Mobility & positioning aids – Int ersecti ons (& over lap ?) w ith ECLSS and TA07 – Critical requirements drivers and enablers for noted technologies in PGA, PLSS, PAS Some Areas Need More Definition Need Approach Path to flight Time? Cost? Value? Better / faster pressure garment development Enhanced suit / human computer models Validated - Applied - ??? ? ? Y Identify, evaluate, integrate, test, multifunctional Coupon tests, ground tests, integrated More effective suits - lower mass, lower materials flight tests N? N? Y expendables, less injury, more durable… Game changing architectures, suit configurations and mobility elements - using Adv.Mat ??????? ? ? Y LEA suits donned extremely quickly, integrated crew escape & crew survival , suit restraint, seat interface & support. ??????? ??????? N? ? Y Long duration suited ops in contingency - waste management, food & drink, etc. ??????? ??????? ? ? Y ?????? (Solutions apply to different Better emergency