Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX RUTGERS.

Slides:



Advertisements
Similar presentations
>ENTER< [PLS PUT ON SAFETY HELMETS BEFORE ENTERING THIS SITE.]
Advertisements

Concept Overview for 2 mt Case “2 mt case”: integrated payloads of no more than 2 mt can be landed on the surface of Mars; extension of current Mars EDL.
Lunar Landing GN&C and Trajectory Design Go For Lunar Landing: From Terminal Descent to Touchdown Conference Panel 4: GN&C Ron Sostaric / NASA JSC March.
Presented by Marco Christov at the 11th Mars Society Annual Convention, 14 – 17 August 2008, Boulder Colorado. A Mars Heavy Transport.
Space Exploration Mars Rovers, Apollo program, Voyager satellites, and SETI All Presented by the Peter C Period: 2 (two) As in 1+1=2 Or 2x1=2 ®
National Aeronautics and Space Administration Presentation to the NASA Goddard Academy 2. Constellation Overview Ken Davidian Lead, Commercial.
NNJ09BH0123RAppendix L A-Crew, Robotics, Avionics, and Vehicle Equipment (CRAVE)- Unrestricted Data Attachment L-2-A-1.
Classroom Addition Facility Planning funds to study a possible addition Enrollment Projections Increase capacity for 2300 students Program includes 19.
1 Architecture and Planning Strategies for Addressing Radiation, Space Weather, and Space Climatology Impact on NASA Missions Study Sponsor - NASA Office.
GSFC/Wallops Flight Facility 1 Small Satellite Opportunities at Wallops Flight Facility Dr. John Campbell Director, Wallops Flight Facility.
Architecture Team Industry Day Briefing 17 January, 2002.
Wind Turbine Towers for Greater Hub Heights Why higher wind turbine tower can contribute to increase energy output? Energy output is proportional to the.
ROVER EGRES S DESIGN Hahna Alexander Anton Galkin Zack Morrison Mobile Robot Design – Fall 2011.
Detail Federal Disaster Housing Assistance Programs Identity various interim housing strategies available to local communities Explain wrap around services.
Astronaut-Aided Construction of a Large Lunar Telescope Background Concepts for large astronomical facilities to follow the Next Generation Space Telescope.
Minimalist Human Mars Mission Surface infrastructure discussion July 26 th, 2008.
Waypoints. 2-Dec-04 USC 2004 AME 557 Space Exploration Architecture Requirements for Waypoints  Located along race path  Provide rovers with supplies.
Settlement Site Selection and Exploration Through Hierarchical Roving Gregory Konesky SGK Nanostructures, Inc. Rutgers Symposium on Lunar Settlements Rutgers.
Earth-Moon Transport Doroteo Garcia Kazuya Suzuki Patrick Zeitouni.
Delivery Systems Joseph T. Wunderlich, Ph.D.. APOLLO 11 SATURN V ROCKET LUANCH VIDEO :
Communication and Navigation System Doro Gracia Kazuya Suzuki Patrick Zeitouni.
Chapter 3 : Distributed Data Processing
Chapter 3 : Distributed Data Processing
Cylindrical Habitats - Horizontal or Gary C. Fisher The Mars Foundation Rutgers University Symposium On Lunar Settlements Piscataway,
Navigation Systems for Lunar Landing Ian J. Gravseth Ball Aerospace and Technologies Corp. March 5 th, 2007 Ian J. Gravseth Ball Aerospace and Technologies.
Habitat & Waypoints Picture. 2-Dec-04 USC 2004 AME 557 Space Exploration Architecture Design Requirements: A safe, reliable, low maintenance habitat to.
Flags Courtesy of 3dflags.com Robotic Precursor Missions to the Moon and Mars Douglas. A. Craig Tetsuji Yoshida NASA- HQ Shimizu Corp. November 2008.
Reducing the cost of sustained operations through technology infusion April 2004 Darin Skelly NASA Kennedy Space Center Transformational Spaceport & Range.
By : PHILLIP, ANGUS, DASHAUN, JORDAN, AND MARCUS.
Strategic Plan Elements: ISRU, Analog Outpost Mike Duke November 10, 2008.
Algorithm Implementation: Safe Landing Zone Identification Presented by Noah Kuntz.
Jet Propulsion Laboratory California Institute of Technology National Aeronautics and Space Administration National Aeronautics and Space Administration.
2 ISS Expansion Utilizing Bigelow Modules Earth Station: Global ISS Marketing – Future of Human Spaceflight Krystal Puga
November 30, 2006 Space Telescope Science Institute Conference Scott “Doc” Horowitz Associate Administrator NASA Exploration Systems Mission Directorate.
Space Power Facility (SPF) CEV Environmental Qualification Testing DISCLAIMER: This Initial Government Concept does not represent a preferred Government.
100% of B-TOS architectures have cost increase under restrictive launch policy for a minimum cost decision maker Space Systems, Policy, and Architecture.
Challenges & Strategies for Lunar Habitation Systems Larry Toups Advanced Projects Office Constellation Program October 2006.
Infrastructure for Reusable Vehicles The next generation of Space Travel Eric Jensen ASTE 527 Infrastructure for Reusable Vehicles The next generation.
MIT : NED : Mission to Mars Presentation of proposed mission plan
RASC-AL 2010 Topics. TECHNOLOGY-ENABLED HUMAN MARS MISSION NASA is interested in eventual human mission to the Martian surface. Current Mars design reference.
Minimalist Mars Mission Establishing a Human Toehold on the Red Planet Executive Summary DevelopSpace MinMars Team.
Mars Today 1 An immediate and inexpensive program for manned Mars visitation.
Overview Problem Solution Advantages Disadvantages Conclusion.
Introduction to the Altair Project
Spacecraft: A vehicle or device designed for travel or operation outside earth’s atmosphere.
Universal Chassis for Modular Ground Vehicles University of Michigan Mars Rover Team Presented by Eric Nytko August 6, 2005 The 2 nd Mars Expedition Planning.
Unit 6 Lesson 1 Explanation. In 2004, President Bush set the following goal for the NASA constellation program, “this vision… is a sustainable and affordable.
Human Exploration of Mars Design Reference Architecture 5
Florida Space Transportation Infrastructure Planning Mark Bontrager Vice President, Spaceport Operations.
National Aeronautics and Space Administration Marshall Space Flight Center Launching the Future of Exploration and Science Robert Lightfoot.
Roadmap for Long Term Sustainable Space Exploration and Habitation Defining the Functional Requirements for Early Phase of Space Habitation AIAA 2015-????
0 Space Exploration and International Cooperation Gilbert R. Kirkham Office of External Relations June 2004.
Crew Mobility for Lunar Surface Exploration Dr. Rob Ambrose NASA-JSC May 2008.
Review of Past and Proposed Mars EDL Systems. Past and Proposed Mars EDL Systems MinMars Mars entry body design is derived from JPL Austere Mars entry.
Approved For Public Release © The Aerospace Corporation 2009 June 17, 2009 Initial Summary of Human Rated Delta IV Heavy Study Briefing to the Review of.
October, 2005 NASA’s Exploration Architecture. 2 A Bold Vision for Space Exploration  Complete the International Space Station  Safely fly the Space.
Affording Mars II: October, 2014 Turning Vision into Reality Humans to Mars Summit May, 2016 George Washington University Washington,
SLS Derived Vertical Habitat
National Goals and Objectives
Water-tube Boilers Description of water tube boilers including operation, types and benefits. A brief synopsis on how they are applied to combined heat.
Callisto Mission LaRC Option
h t t p : / / w w w . u s c . e d u / g o / t t c
What is Facility Layout?  The layout facility is the physical location of the various departments/units of the facility within the premises of the facility.
Mars Sustainability Workshop Kennedy Space Center February 8, 2018
Sustainable Space Development
Space Technology and History
Introduction to the Altair Project
SPLITTING THE ATOM TO CONNECT THE PLANETS
Copyright ©2016 Cengage Learning. All Rights Reserved
Presentation transcript:

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX RUTGERS SYMPOSIUM ON LUNAR SETTLEMENTS 3-8 JUNE 2007 RUTGERS UNIVERSITY Surface Infrastructure Planning and Design Considerations for Future Lunar and Mars Habitation

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX Launch Systems Heavy Lift Vehicles (HLVs) with capabilities to launch payloads approaching 100MT and 7 meter diameter Approaches that utilize Medium Lift Vehicles (MLVs) with capacities ranging from about 15MT to somewhat less than 100MT

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX Lander Considerations Typical Lander Concept SICSA Lander Concept

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX Module Options 1.Conventional module 2.Telescopic module 3.Vertical module with a spherical inflatable section

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX Vertical Module Configurations A triangular pattern scheme affords certain advantages and disadvantages: Pros: A relatively compact configuration footprint at the entry airlock level can minimize the area for site surface preparation if required. Loop egress is achieved with three modules. Con: May be more difficult to position/ assemble. A rectilinear scheme also offers advantages/ disadvantages: Pros: Greater spacing between berthing locations affords more useful wall/ equipment space. Con: Larger footprint for good site selection and/ or surface preparation. 4 modules are needed for loop egress.

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX Combination Configurations The triangular scheme offers advantages and disadvantages: Pros: A very compact footprint around the inflatable module support bases to minimize site surface preparation requirements. Loop egress is achieved with 3 inflatable modules. Con: May be more difficult to assemble. The cruciform scheme also offers advantages and disadvantages: Pros: The deployment footprint around the horizontal module is quite small, limiting site preparation. The scheme can begin as a cruciform and evolve into a closed-loop plan. Con: Dual egress is not achieved until 4 modules are in place.

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX Configuration Comparisons Space/Launch Efficiency

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX Configuration Comparisons Emergency Egress

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX Configuration Comparisons Module Commonality

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX Configuration Comparisons Evolutionary Growth

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX Configuration Comparisons Surface Positioning

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX Inflatable Upper Level Plan Sleeping/Private 1.Partitions 2.Bed and storage 3.Table 4.Chair 5.Shelves 6.Privacy curtains

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX Sleeping/Private Accommodations

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX Inflatable Second Level Plan Labs and Crew Workstations –Glovebox –Sample Photography –Lab’s Workstation –Experiment Tanks –Sink/Refrigerator/ Freezer –Fabric Storage

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX Inflatable Lower Level Plan

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX Common Areas

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX Exercise/Medical Area

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX Exercise and Common Area

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX Site Development Considerations 1.Orbital satellite imaging and unmanned precursor surface surveys should be undertaken to determine safe landing locations with appropriate terrain characteristics for base development. Robotic surface investigation and mapping rovers can determine optimized routings between landing and operational locations and deploy beacons. Automated survey/mapping rovers can later work in conjunction with rovers used for power cable deployment and cargo/human transport. 2.Landing sites must be located at sufficient distances from habitats and other sensitive areas. Use of tethered landers can greatly reduce or avoid projectile hazards. RTGs or other power systems that produce radiation safety hazards must be located at a safe distance away from habitable facilities..

Larry Bell, Sasakawa International Center for Space Architecture (SICSA) Gerald D. Hines College of Architecture, University of Houston, Houston TX