Human Factors and Habitability
|
|
|
- Winfred Wilkerson
- 5 years ago
- Views:
Transcription
1 Human Factors and Habitability Discussion of Midterm Required Crew Volumes Human Physiological Adaptation to 0G Workstation Design Restraint Design Ideal Cabin Layout Habitability in Partial Gravity Stowage Extravehicular Activity David L. Akin - All rights reserved
2 Initial Design Review 2:30-4:30 tomorrow (Friday, 10/30) Engineering Annex Building 0307 (in courtyard of A. V. Williams) 2
3 Midterm Exam In-class on Thursday 11/5 Open notes Bring a calculator No computers or cell phones Sample midterm and solutions are posted on spacecraft site 3
4 Mercury Spacecraft Interior Layout 4
5 Gemini 4 Crew Cabin 5
6 Apollo Command Module Interior (port side) 6
7 Apollo Command Module Interior (starboard) 7
8 Apollo Command Module Interior 8
9 Apollo Spacecraft (Rescue Configuration) 9
10 Soyuz Interior 10
11 Apollo Lunar Module Interior (looking fwd) 11
12 Apollo Lunar Module Interior (looking aft) 12
13 Required Habitable Volume (Celentano) Skylab (100 m 3 ) ISS (170 m 3 ) Shuttle + Spacelab Shuttle + Spacehab Shuttle Lunar Module Mercury Apollo Gemini From Nicogossian et. al., Space Biology and Medicine, Vol. II: Life Support and Habitability, AIAA,
14 Historical Data Fitted to Celentano 62 ( ) 1 e t 35 14
15 Curve Fit to Small Hab Data Only 20 ( ) 1 e t 8 15
16 Acoustics From Nicogossian et. al., Space Biology and Medicine, Vol. II: Life Support and Habitability, AIAA,
17 0G Neutral Body Posture From Nicogossian et. al., Space Biology and Medicine, Vol. II: Life Support and Habitability, AIAA,
18 0G Restrained Reach Envelope From Nicogossian et. al., Space Biology and Medicine, Vol. II: Life Support and Habitability, AIAA,
19 Minimum Translation Paths (IVA) 19
20 0G Workstation Layout From Nicogossian et. al., Space Biology and Medicine, Vol. II: Life Support and Habitability, AIAA,
21 Apollo Telescope Mount Training 21
22 Skylab ATM Chair Restraint From MSFC Skylab Crew Systems Mission Evaluation, NASA TM X-64825,
23 Operating ATM On-Orbit 23
24 Skylab Table Restraints From MSFC Skylab Crew Systems Mission Evaluation, NASA TM X-64825,
25 Isogrid Flooring Design From MSFC Skylab Crew Systems Mission Evaluation, NASA TM X-64825,
26 Skylab Orbital Workshop Module 26
27 Cleat Restraint System From MSFC Skylab Crew Systems Mission Evaluation, NASA TM X-64825,
28 Skylab Triangle-Cleat Shoe 28
29 EVA Foot Restraints From MSFC Skylab Crew Systems Mission Evaluation, NASA TM X-64825,
30 Skylab Exterior Configuration 30
31 Skylab Orbital Work Shop Interior 31
32 Skylab Multiple Docking Adapter Layout From MSFC Skylab Crew Systems Mission Evaluation, NASA TM X-64825,
33 Skylab Living Quarters Layout 33
34 Skylab Sleeping Compartments 34
35 Skylab Wardroom Layout From MSFC Skylab Crew Systems Mission Evaluation, NASA TM X-64825,
36 Skylab Wardroom Table 36
37 Skylab Waste Management Compartment 37
38 Stowage Number of items stowed proportional to volume, crew size, duration, complexity of mission Mercury: 48 items Gemini: 196 Apollo: 1727 Shuttle: 2600 Skylab: 10,160 ISS: >20,000 After you stow it, how do you find it? 38
39 Psychosocial Issues Scheduling and planning Recreation Command structure Issues affecting crew morale Environment Food and drink Exercise Hygiene Noise Lighting 39
40 International Space Station 40
41 A Tour of International Space Station 41
42 Analogue Habitats - NR-1 Submarine 42
43 Minimum Functional (Lunar) Habitats 43
44 44
45 Habitat Layout - Vertical or Horizontal? Geometric modeling of packing factor to fit humans into cylindrical shapes Mass estimation for human-rated pressurized volumes from JSC (converted to metric) M < kg >= ( A surface <m 2 > ) Space Systems Laboratory
46 Habitat Layout Trades - Floor Area Mass (kg) Habitable Floor Area (m^2) Vertical, 1 floor Horizontal, L=3 m Horizontal, L=5.5 m Horizontal, L=8 m Vertical, 2 floors Design Point 46 Space Systems Laboratory
47 Habitat Layout Trades - Useful Volume 47 Space Systems Laboratory
48 Habitat Layout Trades - Accessible Wall Mass (kg) Surface-Accessible Wall Length (m) Vertical, 1 floor Horizontal, L=3 m Horizontal, L=5.5 m Horizontal, L=8 m Vertical, 2 floors Design Point 48 Space Systems Laboratory
49 Habitat Layout Trades - Total Volume Mass (kg) Total Interior Volume (m^3) Vertical, 1 floor Horizontal, L=3 m Horizontal, L=5.5 m Horizontal, L=8 m Vertical, 2 floors Design Point 49 Space Systems Laboratory
50 Conclusions From Trades and Designs Minimum functional habitat is feasible across the spectrum of possible designs Inflatable Horizontal cylinder Vertical cylinder An MFH which meets the mass limitations of this study will be quite small Multilayer vertical configuration (clearly favored by parametric analysis) has much less design background (other than colonization concepts) Significant utility to a full-scale mockup for evaluation 50 Space Systems Laboratory
51 Development of Final Design Synthesis from preliminary designs, trade studies, virtual reality, and full-scale mockup tended to 3.65 m diameter Two full-diameter levels Separation of operations and habitation functions Operational assumptions Four suitports for nominal ops plus inflatable airlock Premium on stowage, multipurpose space, functionality Design to MFH specifications for outpost; examine options in both growth (multihabitat) and isolated (self-sufficient habitat) directions 51 Space Systems Laboratory
52 UMd Final MFH Design m diameter 5.5 m tall 4:1 ellipsoidal endcaps Three module berthing ports (Cx standard) Four suitports (two in berthing hatches) Inflatable airlock All 6063-T6 structure Space Systems Laboratory
53 Habitat Orthogonal Views 3.65 m 5.5 m 53 Space Systems Laboratory
54 Lower Deck Layout CTB Stowage Racks Air Handling/ CO2 Scrubbing/ Heat Exchanger Multipurpose Table Berthing Hatch Ladder to Upper Deck 54 Water Recycling Space Systems Laboratory
55 Lower Deck Layout 55 Space Systems Laboratory
56 Upper Deck Layout Individual Crew Berths Galley Wall - Food Preparation Bathroom Table and Seats Opened for Meals; Stowed Otherwise 56 CTB Stowage Racks Space Systems Laboratory
57 Upper Deck Layout 57 Space Systems Laboratory
58 Crew Berths Personal sleeping berths Individual stowage for 6 CTBs and 0.24 m 3 of loose gear Water wall kg of water provides 5 gm/cm 2 radiation shielding (polyethylene door not shown) Contingency waste management for 48 hours 58 Space Systems Laboratory
59 Crew Berths 59 Space Systems Laboratory
60 Partial Gravity Sims of Habitability 60 Space Systems Laboratory
61 Segmented Rover - Inboard Plan View Bhardwaj et. al., Design of a Pressurized Lunar Rover - Final Report NASA CR , Virginia Polytechnic Institute and State University,
62 Segmented Rover - Inboard Profiles Bhardwaj et. al., Design of a Pressurized Lunar Rover - Final Report NASA CR , Virginia Polytechnic Institute and State University,
63 TURTLE Interior Mockup - ENAE
64 Analysis of Sight Lines Bhardwaj et. al., Design of a Pressurized Lunar Rover - Final Report NASA CR , Virginia Polytechnic Institute and State University,
65 Constellation Lunar Surface Architecture 65
Human Factors and Habitability MARYLAND
Human Factors and Habitability Discussion of Midterm and future project work Required Crew Volumes Human Physiological Adaptation to 0G Workstation Design Restraint Design Ideal Cabin Layout Habitability
Habitability (continued)
Habitability (continued) Required Crew Volumes Human Physiological Adaptation to 0G Workstation Design Restraint Design Ideal Cabin Layout Habitability in Partial Gravity Stowage Various Examples 106 2017
Introduction to Habitability
Introduction to Habitability Required Crew Volumes! Human Physiological Adaptation to 0G! Workstation Design! Restraint Design! Ideal Cabin Layout! Habitability in Partial Gravity! Stowage! Various Examples
Water Reclamation MARYLAND. Fundamentals of water reclamation Water reclamation. Solids disposal. Potable Hygiene Urine U N I V E R S I T Y O F
Fundamentals of water reclamation Water reclamation Potable Hygiene Urine Solids disposal 1 2011 David L. Akin - All rights reserved http://spacecraft.ssl.umd.edu ISS Consumables Budget Consumable Design
ENAE 697 Overview and Introduction
ENAE 697 Overview and Introduction Course overview Goals Web-based content Syllabus Policies Project content Overview of space human factors and life support History of humans and flight Brief overview
Crew Systems Project ENAE 483 Fall Team A2: Douglas Astler Stephanie Bilyk Kevin Lee Grant McLaughlin Rajesh Yalamanchili
Crew Systems Project ENAE 483 Fall 2012 Team A2: Douglas Astler Stephanie Bilyk Kevin Lee Grant McLaughlin Rajesh Yalamanchili Presentation Overview Requirements and Assumptions Trade studies and life
Space Simulation MARYLAND U N I V E R S I T Y O F. Space Simulation. ENAE 483/788D - Principles of Space Systems Design
Focus is on human-in-the-loop operational simulations, not component sims (e.g., thermal vacuum chambers) Microgravity Planetary surfaces Specialty simulations A vision and a challenge... 1 2012 David
Space Simulation MARYLAND U N I V E R S I T Y O F. Space Simulation. ENAE 483/788D - Principles of Space Systems Design
Lecture #27 December 4, 2014 Focus of this lecture is on human-in-the-loop operational simulations, not component sims (e.g., thermal vacuum chambers) Microgravity Planetary surfaces Specialty simulations
Crew Systems Design Project Group A8. Chrissy Doeren Kip Hart Kiran Patel Alex Slafkosky
Crew Systems Design Project Group A8 Chrissy Doeren Kip Hart Kiran Patel Alex Slafkosky Project Overview Objective: design a crewed spacecraft for a low cost lunar mission Crew: 3-95th percentile men Duration:
Crew Systems Analysis for 10-Day Round-Trip to Moon
Crew Systems Analysis for 10-Day Round-Trip to Moon Ben Abresch Matt Marcus Sean Robert Nick Zarbo 10/18/2012 Mission Requirements 10 day nominal trip 3 contingency days Crew systems mass
A Dual-Chamber Hybrid Inflatable Suitlock (DCIS) for Planetary Surfaces or Deep Space
41st International Conference on Environmental Systems 17-21 July 2011, Portland, Oregon AIAA 2011-5064 A Dual-Chamber Hybrid Inflatable Suitlock (DCIS) for Planetary Surfaces or Deep Space A. Scott Howe,
Space Simulation and Human Testing
Space Simulation and Human Testing Focus is on human-in-the-loop operational simulations, not component sims (e.g., thermal vacuum chambers) Microgravity Planetary surfaces Specialty simulations Human
ENAE483 Project 1. David Nestor Skylar Trythall Matt Vaughn Ryan Quinn
ENAE483 Project 1 David Nestor Skylar Trythall Matt Vaughn Ryan Quinn 9. Con-ops Outline 1. Transport Design 2. Transport Interior Design 3. Life Support and Logistics for Transport Design 4. Habit Design
Modular Mars Analog Settlements. 2013, 2017 Kent Nebergall, All Rights Reserved.
Modular Mars Analog Settlements BEYOND THE LANDER KENT NEBERGALL Lander versus Settlement Analog Goals Lander Analog Goals High Fidelity to Space-X MCT form factor (10 M Cylinder) Micro-Settlement Analog
IAC-06-D4.1.2 CORRELATIONS BETWEEN CEV AND PLANETARY SURFACE SYSTEMS ARCHITECTURE PLANNING Larry Bell
IAC-06-D4.1.2 CORRELATIONS BETWEEN CEV AND PLANETARY SURFACE SYSTEMS ARCHITECTURE PLANNING Larry Bell Sasakawa International Center for Space Architecture (SICSA), University of Houston, USA e-mail: lbell@uh.edu
Preliminary Design Review
Crew Systems and Life Support Establishing a Recurring Human Presence on the Moon Preliminary Design Review Overview Preliminary Design Review of Crew Systems / Life Support aboard low-cost lunar lander
A Modular Habitation System for Human Planetary and Space Exploration
45th 12-16 July 2015, Bellevue, Washington Paper Number A Modular Habitation System for Human Planetary and Space Exploration A. Scott Howe, PhD 1 Jet Propulsion Laboratory, California Institute of Technology,
Extravehicular Activity
Lecture #24 November 21, 2017 Full pressure suits and high-altitude aviation Early human space program Operational suits Interfaces to habitats and rovers Spacesuit alternatives 1 2017 David L. Akin -
Preliminary Cost Analysis MARYLAND. Cost Sources Vehicle-level Costing Heuristics Applications Learning Curves Program-Level Analysis
Cost Sources Vehicle-level Costing Heuristics Applications Learning Curves Program-Level Analysis 2003 David L. Akin - All rights reserved http://spacecraft.ssl.umd.edu Cost Analysis Direct Costs - directly
Human Spaceflight Laboratory
Human Spaceflight Laboratory Moon Mars Beyond The Human Spaceflight Laboratory in the Department of Space Studies T he University of North Dakota s Space Studies Department, in the John D. Odegard School
Altair Constellation Returns Humans to the Moon
Altair Cover Page Altair Constellation Returns Humans to the Moon Clinton Dorris Deputy Manager Altair Project Office Constellation EXPLORATION ROADMAP 05 06 07 08 09 10 11 12 13 14 15 16 17 18 19 20 21
EVA OFFICE EXTRAVEHICULAR ACTIVITY (EVA) AIRLOCKS AND ALTERNATIVE INGRESS/EGRESS METHODS DOCUMENT
National Aeronautics and Space Administration EVA-EXP-0031 BASELINE EFFECTIVE DATE: 04/18/2018 EVA OFFICE EXTRAVEHICULAR ACTIVITY (EVA) AIRLOCKS AND ALTERNATIVE INGRESS/EGRESS METHODS DOCUMENT Release
Trade and Analysis Study for a Lunar Lander Habitable Module Configuration
40th International Conference on Environmental Systems AIAA 2010-6134 Trade and Analysis Study for a Lunar Lander Habitable Module Configuration Marc M. Cohen 1 Northrop Grumman Corporation, El Segundo
Fundamentals of Decompression
History Tissue models Haldane Workman Bühlmann Physics of bubbles Spacecraft cabin atmospheres 1 2011 David L. Akin - All rights reserved http://spacecraft.ssl.umd.edu First Class Assignment Four topics
Lecture 4: Spaceflight Environment
Space Environment and Effects Previous Lecture Next Lecture Home Classes Contact Lecture 4: Spaceflight Environment 1. Gravity (see Lecture 3): Microgravity, Microgravity Simulation Launch / Landing Acceleration
Loads, Structures, and Mechanisms. Team C5 Matthew Marcus Chris O'Hare Alex Slafkosky Scott Wingate
Loads, Structures, and Mechanisms Matthew Marcus Chris O'Hare Alex Slafkosky Scott Wingate Presentation Overview Design requirements Initial crew capsule design choice Pressure vessel design Pressure loads
Japanese Experiment Module ( JEM)
The Space Congress Proceedings 1986 (23rd) Developing Space For Tomorrow's Society Apr 1st, 8:00 AM Japanese Experiment Module ( JEM) Takehiko Kato Japan Liaison for Space Station Program National Space
NanoRacks/Quad-M Rideshare Overview. Michael D. Johnson 10/12/2016
NanoRacks/Quad-M Rideshare Overview Michael D. Johnson 10/12/2016 Why NanoRacks/Quad-M Team? NRCSD Kaber Cygnus External Deployer NREP NR Airlock Dragon Trunk Deployer Centaur Aft Bulkhead Deployer Centaur
CONSTELLATION PROGRAM HUMAN-SYSTEMS INTEGRATION REQUIREMENTS
CxP 70024 BASELINE National Aeronautics and Space Administration RELEASE DATE: DECEMBER 15, 2006 CONSTELLATION PROGRAM HUMAN-SYSTEMS INTEGRATION REQUIREMENTS ADL: The applicable and reference documents
Robotic On-Orbit Satellite Servicing: One Size Does Not Fit All
Robotic On-Orbit Satellite Servicing: One Size Does Not Fit All Dr. David L. Akin Dr. Craig R. Carignan Space Systems Laboratory On-Orbit Servicing Demand by Types Reboost Inspection Dexterous Servicing
V.E.G.E.T.A.B.L.E. Melissa Adams, Dylan DiBernardo, Caleb Fricke, Dale Martin, Christopher Moseman, Luke Renegar
V.E.G.E.T.A.B.L.E. The Variable Environmental Gravity Exploration Transit Accommodation with Baseline Landing Extension Melissa Adams, Dylan DiBernardo, Caleb Fricke, Dale Martin, Christopher Moseman,
STAR European Conference 2011
STAR European Conference 2011 Oggetto: Data: Aircraft passenger cabin thermal comfort analysis by means of integrated mono dimensionałcfd approach 22-23 March 2011 Ver.: P. Borrelli, On Board General Systems,
Neutral Buoyancy Laboratory: Astronauts from the Pool to Spacewalks Kurt Otten, BSEE
Denver, CO October 18-20, 2017 Neutral Buoyancy Laboratory: Astronauts from the Pool to Spacewalks Kurt Otten, BSEE Kurt Otten is the Operations Manager for NASA s Neutral Buoyancy Laboratory (NBL) in
ETHOS Environmental and Thermal Operating Systems (ETHOS)
ISS Live! was developed at NASA s Johnson Space Center (JSC) under NASA Contracts NNJ14RA02C and NNJ11HA14C wherein the U.S. Government retains certain rights. Console Handbook ETHOS Environmental and
USS ALABAMA BATTLESHIP MEMORIAL PARK. Vocabulary
USS ALABAMA BATTLESHIP MEMORIAL PARK Vocabulary The following terms are common vocabulary for ships including battleships and submarines, like the USS ALABAMA and USS DRUM. ACOUSTIC - Means "sound" as
PRELIMINARY DESIGN STUDY OF LUNAR HOUSING CONFIGURATIONS
PRECEDff_'G P_GE BLANK NOT F_LMtED PRELMNARY DESGN STUDY OF LUNAR HOUSNG CONFGURATONS... 93- K. H. Reynolds jr. O. Box 1021 McLean VA 22101 17443 255 A preliminary design study assesses various configurations
JSC/EC5 U.S. Spacesuit Knowledge Capture (KC) Series Synopsis. This synopsis provides information about the Knowledge Capture event below.
JSC/EC5 U.S. Spacesuit Knowledge Capture (KC) Series Synopsis All KC events will be approved for public using NASA Form 1676. This synopsis provides information about the Knowledge Capture event below.
Pressurized Rover Airlocks SAE TECHNICAL PAPER SERIES. Marc M. Cohen NASA-Ames Research Center
SAE TECHNICAL PAPER SERIES 2000-01-2389 Pressurized Rover Airlocks Marc M. Cohen NASA-Ames Research Center 30 th International Conference on Environmental Systems Toulouse, France July 10-13, 2000 400
Avionics System Project. Team D3 Dylan Carter, Jesse Cummings, Kenneth Murphy, Rajesh Yalamanchili
Avionics System Project Team D3 Dylan Carter, Jesse Cummings, Kenneth Murphy, Rajesh Yalamanchili Link Budgets for Communication Communication needs during the mission are divided into distinct phases,
The Metal Shark 75 Endurance is a welded aluminum pilothouse catamaran specially designed for use as a law enforcement, port security, and fire
The Metal Shark 75 Endurance is a welded aluminum pilothouse catamaran specially designed for use as a law enforcement, port security, and fire rescue response boat. Like all Metal Sharks, it may be fully
Exploration Systems Mission Directorate
Exploration Systems Mission Directorate Lunar Architecture Update AIAA Space 2007 September 20, 2007 NASA s Lunar Architecture Introduction to Session Doug Stanley Current exploration strategy and status
Presentation Contents
OTOS Presentation Contents Mission Requirements Mission Operations Architecture Design Reference Missions Habitat Configuration CONOPS Life Support Contingency Accommodations Plans for Experimental Testing
r bulletin 98 june 1999 bull
r bulletin 98 june 1999 bull ESA s contributions to the ISS. MPLM is highlighted in pink; the other ESA-provided items for Partner elements are in light blue. Right: MPLM remains berthed only while the
ICES HISTORY PANEL SPACE SUIT DEVELOPMENT
ICES HISTORY PANEL SPACE SUIT DEVELOPMENT Mercury Gemini Apollo James McBarron II July 9, 2007 1 SPACE SUIT DEVELOPMENT AGENDA LITTLE KNOWN DETAILS ABOUT - SPACE SUIT & CONTRACTOR SELECTION - SOME LESSONS
Complex operations on the International Space Station training and execution in manned and unmanned situations
Complex operations on the International Space Station in manned and unmanned situations Uwe.Muellerschkowski@esa.int Outline What makes ISS operations complex Operations based on procedures Astronaut training
Between the Market and the Moon Requirements for Lunar Tourism
Between the Market and the Moon Requirements for Lunar Tourism Eric Dahlstrom InternationalSpace.com Emeline Paat-Dahlstrom Space Adventures, Ltd. 20 September 2005 International Lunar Conference Toronto,
Crew Protection, Contingency EVA and the Crew Exploration Vehicle
2006-01-2137 Crew Protection, Contingency EVA and the Crew Exploration Vehicle Copyright 2006 SAE International Gary L. Harris, Pablo de León Department of Space Studies, University of North Dakota ABSTRACT
Aerospace Physiology. Lecture #11 Oct. 7, 2014 Cardiopulmonary physiology. Musculoskeletal Vestibular Neurological Environmental Effects MARYLAND
Lecture #11 Oct. 7, 2014 Cardiopulmonary physiology Respiratory Cardiovascular Musculoskeletal Vestibular Neurological Environmental Effects 1 2014 David L. Akin - All rights reserved http://spacecraft.ssl.umd.edu
Post 42 Convertible YACHTS OF QUALITY, NOT QUANTITY SINCE A Tradition Of Excellence For Nearly Half A Century.
Post 42 Convertible YACHTS OF QUALITY, NOT QUANTITY SINCE 1957 A Tradition Of Excellence For Nearly Half A Century. Post 42 Convertible Is A Handcrafted, Beautifully Mannered Yacht. There isn t a yacht
USS Charles F Adams DDG-2 Philadelphia Open House. May 17-18, 2010
USS Charles F Adams DDG-2 Philadelphia Open House May 17-18, 2010 Starboard Side P1000506 Port side looking aft 39 radar is bolted to a bracket that is welded to the main deck. Note that the air vents
Assembly Instructions for STS-110 payload
2008 Assembly Instructions for STS-110 payload IMPORTANT NOTE TO MODELERS The making of this model requires the use of the X-acto knife (craft knife) and tweezers, besides a simple scissor. Also important,
Space Suits: An Evolution of Protection
Space Suits: An Evolution of Protection Throughout the history of space exploration, back through to the very first sparks of imagination, space suits have been a way to protect our bodies from the dangers
www.leopardcatamarans.com introducing An elegant breed of catamaran The Leopard 44 represents Robertson & Caine s innovative developments with modern features not yet seen on production catamarans, while
EUROBOT END-EFFECTORS
In Proceedings of the 8th ESA Workshop on Advanced Space Technologies for Robotics and Automation 'ASTRA 2004' ESTEC, Noordwijk, The Netherlands, November 2-4, 2004 EUROBOT END-EFFECTORS S.Michaud (1),
Preface...xxiii Introduction...xxv About the Editors...xxvii About the Contributors... xxxi
Contents Preface...xxiii Introduction...xxv About the Editors...xxvii About the Contributors... xxxi CHAPTER 1 Introduction to Space Safety... 1 1.1 NASA and Safety... 2 1.2 Definition of Safety and Risk...
Integrating Life Science, Engineering & Operations Research to Optimize Human Safety and Performance in Planetary Exploration
Integrating Life Science, Engineering & Operations Research to Optimize Human Safety and Performance in Planetary Exploration Mike Gernhardt August 20, 2009 The Challenge of Moving Past Apollo Apollo was
Traveling and Working in Space
Traveling and Working in Space Read the information provided in Traveling and Working in Space. Decide if each statement below is true or false. Write the word in the blank before each statement. If the
Bathroom master cabin. Master cabin with private terrace & bathing platform
SWAN 105 TI-COYO was commissioned by an experienced owner who sought a modern performance cruiser utilizing the very latest technology while maintaining a high level of comfort and the ability to sail
SY WHIRLWIND OF ST PETERS PORT
SY WHIRLWIND OF ST PETERS PORT Holland Jachtbouw, Netherlands - 27.43 m Yacht Type: Cruising Sailboat Captain & Crew: 4 LOA: 27.43 m / 90' 0'' Guest cabins: 3 Cruising speed: 9 knots Guests sleeping: 6
New Azimut Magellano 66. Preliminary presentation
New Azimut Magellano 66 THIS DOCUMENT IS VALID AS A PRELIMINARY PRESENTATION ONLY This brochure in no way constitutes a contract of sale for the boatyard s vessels to any person or company. All information
An innovative, contemporary catamaran
Designer/Builders Robertson & Caine and Naval Architects Simonis-Voogd have set a new standard for contemporary cruising catamarans with the launch of the Leopard 40. The innovative interior layout, increased
Slide 1 / What is the density of an aluminum block with a mass of 4050 kg and volume of 1.5 m 3?
Slide 1 / 68 1 What is the density of an aluminum block with a mass of 4050 kg and volume of 1.5 m 3? Slide 2 / 68 2 What is the mass of a rectangular shaped ice block with dimensions of 0.04m x 0.05m
Extravehicular Activity (EVA) Life Support System (LSS)
ISS Live! was developed at NASA s Johnson Space Center (JSC) under NASA Contracts NNJ14RA02C and NNJ11HA14C wherein the U.S. Government retains certain rights. Extravehicular Activity Console Position:
3. How many kilograms of air is in the room?
1. Astronomers use density as a clue to the composition of distant objects. Judging by the orbits of its moons the mass of Saturn is found to be 5.68 10 26 kg. (a) Use its mean radius 58 230 km to determine
Risk Management Considerations of the SOFIA Aircraft
Risk Management Considerations of the SOFIA Aircraft Michael V. Frank, Ph.D., P.E., CMC riskexpert@ieee.org Reliable, SFASafe, Affordable Technology SOFIA Project Overview Create a Stratospheric Observatory
SSC15-II-6. payload), allowing a new class of larger deployable payloads to utilize the ISS as a research platform.
SSC15-II-6 Paving the Way for Small Satellite Access to Orbit: Cyclops Deployment of SpinSat, the Largest Satellite ever Deployed from the International Space Station Matthew P. Hershey, Daniel R. Newswander,
Integrating Life Sciences, Engineering & Operations Research to Optimize Human Safety and Performance in Planetary Exploration
Integrating Life Sciences, Engineering & Operations Research to Optimize Human Safety and Performance in Planetary Exploration Mike Gernhardt August 20, 2009 The Challenge of Moving Past Apollo Apollo
Design Germán Frers This new design was created practically simultaneously with the Swan 78 as a complement to the larger sister of the new bluewater
Design Germán Frers This new design was created practically simultaneously with the Swan 78 as a complement to the larger sister of the new bluewater line of yachts. The size seems to be a very popular
Pulmonary (cont.) and Decompression
Pulmonary (cont.) and Decompression Respiratory deficiencies Emergency and explosive decompression Denitrogenation and decompression sickness Tissue models Physics of bubble formation Atmosphere constituent
DUFOUR CATAMARANS 48 Launch of a new tenor
DUFOUR CATAMARANS - PRESS RELEASE - DECEMBER 2017 DUFOUR CATAMARANS 48 Launch of a new tenor It is true then? The rumor was spread in the last few months... Well, yes! Dufour is proud to announce its entry
Measuring Lung Capacity
Name Class Date Chapter 37 Circulatory and Respiratory Systems Measuring Lung Capacity Introduction The amount of air that you move in and out of your lungs depends on how quickly you are breathing. The
Next Generation Life Support (NGLS): Variable Oxygen Regulator Element
ABSTRACT The Variable Oxygen Regulator is a new technology to provide pressure control for the next generation space suit. Using a motor-driven actuator, this dual-stage regulator allows, for the first
Code of safe practice for cargo stowage and securing Annex 14
(Dec 2013) Code of safe practice for cargo stowage and securing Annex 14 M.1/Circ.1352 Annex - Amendments to the Code of Safe Practice for Cargo Stowage and Securing (CSS Code): Annex 14 Guidance on Providing
International Space Station Acoustic Noise Control - Case Studies
International Space Station Acoustic Noise Control - Case Studies Ferdinand W. Grosveld, 362 North First Street Hampton, Virginia 23664 noisecon@grosveld.com Jerry R. Goodman Lyndon B. Johnson Space Center
WHITE CAPS. Billy Black
WHITE CAPS LOA 42.3, Beam 14.4, Draft 3.8 Displacement 29000 lb (fully loaded) Owners: Harvey and Judy White Designer: Sabre Design Team Built 2006 by Sabre Yachts, South Casco, Maine The owners of White
Barge Dutch Barge. Medway United Kingdom. 125,000 inc Vat. Spits barge for sale
Barge Dutch Barge Precious Marine - Woolverstone Marina, Woolverstone, Ipswich, Suffolk, IP9 1AS - www.preciousmarine.co.uk - +44 (0)1473 780286 - info@preciousmarine.co.uk Barge Dutch Barge Medway United
Atmospheres and Decompression
Atmospheres and Decompression Emergency and explosive decompression Denitrogenation and decompression sickness Tissue models Physics of bubble formation Atmosphere constituent analysis 1 2017 David L.
Advanced EVA Helmet Assembly
44th 13-17 July 2014, Tucson, Arizona ICES-2014-193 Advanced EVA Helmet Assembly Michael H. McCarthy 1 and Brian Battisti 2 Air-Lock, Incorporated, Milford, CT, 06460 Travis Ripps 3 David Clark Company
PRELIMINARY Presented at the SLSD 7S SORR 9/9/03
PRELIMINARY Presented at the SLSD 7S SORR 9/9/03 Space and Life Sciences Directorate ISS Flight 7 Soyuz Stage Operations Readiness Review Certification of Flight Readiness September 24, 2003 J. B. Walters
Water Immersion Ballasted Partial Gravity for Lunar and Martian EVA Simulation
2007-01-3145 Water Immersion Ballasted Partial Gravity for Lunar and Martian EVA Simulation Copyright 2007 SAE International John Mularski and David L. Akin Space Systems Laboratory, University of Maryland
BOEING AIRCRAFT WEIGH WORKSHEET
WEIGHING FACILITIES AND EQUIPMENT ITEM MECH INSP The airplane should be weighed inside a closed facility that will: Exclude all wind and drafts. Permit shutdown of air conditioning during the weighing
Design Germán Frers This new design was created practically simultaneously with the Swan 78 as a complement to the larger sister of the new bluewater line of yachts. The size seems to be a very popular
A Liter a Lung Measuring Lung Capacity
A Liter a Lung Measuring Lung Capacity OBJECTIVE In this investigation, students will compare the actual and expected vital capacities of their classmates. LEVEL Middle Grades Life Science CONNECTIONS
www.leopardcatamarans.com DISCOVER An innovative, contemporary catamaran Designer/Builders Robertson & Caine and Naval Architects Simonis-Voogd have set a new standard for contemporary cruising catamarans
Aerospace Physiology. Lecture #10 Oct. 6, 2015 Cardiopulmonary physiology. Musculoskeletal Vestibular Neurological Environmental Effects MARYLAND
Lecture #10 Oct. 6, 2015 Cardiopulmonary physiology Respiratory Cardiovascular Musculoskeletal Vestibular Neurological Environmental Effects 1 2015 David L. Akin - All rights reserved http://spacecraft.ssl.umd.edu
Schock Harbor 25 Sempre Amici
Schock Harbor 25 Sempre Amici Make: Schock Model: Harbor 25 Length: 25 ft Price: $ 62,000 Year: 2009 Condition: Used Location: Seattle, WA, United States Boat Name: Hull Material: Draft: Number of Engines:
New High School #6. Schematic Design Presentation. Killeen Independent School District \\ Killeen, Texas. October 09, 2018
New High School #6 Killeen Independent School District \\ Killeen, Texas Schematic Design Presentation October 09, 2018 SCHEMATIC DESIGN SITE / FLOOR PLANS 1 Schematic Design Images SCHEMATIC SITE PLAN
American Institute of Aeronautics and Astronautics
42nd International Conference on Environmental Systems 15-19 July 2012, San Diego, California AIAA 2012-3558 Inflatable Land Shelter Demonstrator Nathan Wong 1 and Ondrej Doule, Ph.D. 2 International Space
Horizontal Bladder Tanks
DATA SHEET Horizontal Bladder Tanks Features UL Listed and FM Approved for use with various ANSUL proportioners and foam concentrates 175 psi (12.1 bar) maximum allowable working pressure (design pressure)
Structural Design, Analysis, and Testing of an. Expandable Lunar Habitat
50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference17th 4-7 May 2009, Palm Springs, California Visit the SIMULIA Resource Center for more customer examples. AIAA 2009-2166
HERITAGE, VINTAGE AND CLASSIC YACHTS +44 (0) MOODY LANCER - SOLD. Specification COME TRUE MOODY LANCER. 38 ft 6 in / 11.
HERITAGE, VINTAGE AND CLASSIC YACHTS +44 (0)1202 330 077 MOODY LANCER - SOLD COME TRUE MOODY LANCER Designer Length waterline 38 ft 6 in / 11.73 m Engine Perkins 190hp 2xDiesel Builder Tyler Boat Co Ltd
WILD TIMES WILD FISH Sportsfishing in remote PNG
CLUB MARINE Vol. 30 No. 3 June-July 2015 Vol. 30 No. 3 AUSTRALASIA S LEADING MARINE LIFESTYLE MAGAZINE WILD TIMES WILD FISH Sportsfishing in remote PNG Print Post Approval PP327855100004. RRP $10.95 DALY
14,950 Tax Paid. Moody over 700 boats listed CHICHESTER OFFICE OFFICES THROUGHOUT THE UK AND EUROPE
CHICHESTER OFFICE OFFICES THROUGHOUT THE UK AND EUROPE Moody 29 Year: 1983 Heads: 1 Location: Dell Quay Nr Chichester Cabins: 2 LOA: 29' 8" (9.04m) Berths: 6 Beam: 10' 6" (3.20m) Keel: Fin keel Min Draft:
hainesmarine.co.uk Haines 26
hainesmarine.co.uk Haines 26 Haines 26 HAINES MARINE Unlike mass production builders Haines combine traditional craftsmanship with modern techniques and will tailor a boat to individual requirements. Ordering
Rocky Captain Users Manual
Rocky Captain Users Manual 5/13/14 rev 3 pg Table of Contents LEROY (INFLATABLE DINGHY) 3 FLOAT PLAN 3 AIR 3 YAMAHA ENGINE 5 GASOLINE 5 CONTROLS FOR OPERATING ENGINE 6 TIE- OFF 10 MAINTENANCE 11 ROCKY
Feasibility of Developing a Refrigerant-Based Propulsion System for Small Spacecraft
Feasibility of Developing a Refrigerant-Based Propulsion System for Small Spacecraft Carl Seubert, et al. Small Satellite Conference August 14 th 2007 Outline Background Propulsion system requirements
Vertical Bladder Tanks
DATA SHEET Vertical Bladder Tanks Features UL Listed and FM Approved for use with various ANSUL proportioners and foam concentrates 175 psi (12.1 bar) maximum allowable working pressure (design pressure)
An elegant breed of catamaran
Founded upon the ethos of continuous innovation, and with careful consideration to feedback from cruising and charter clients, the Leopard 45 represents astute value, elegant lines and satisfies blue water
Space Suit Concepts and Vehicle Interfaces for the Constellation Program
Publications 7-9-2007 Space Suit Concepts and Vehicle Interfaces for the Constellation Program D. M. Klaus University of Colorado Boulder J. Metts University of Colorado Boulder R. Kobrick University of
57 Riviera 575 SUV 2016
The SUV collection is a culmination of more than 32 years of boat building design, experience and extensive owner feedback from around the world. Bearing Riviera s classic hallmark design, the new 575