ALBERT

All Library Books, journals and Electronic Records Telegrafenberg

X
feed icon rss

Your email was sent successfully. Check your inbox.

An error occurred while sending the email. Please try again.

Proceed reservation?

Export
  • 1
    facet.materialart.
    Unknown
    Multi Purpose Crew Vehicle Environmental Control and Life Support Development Status (2012)
    In:  CASI
    Details
    Publication Date: 2019-07-19
    Description: The Orion Multi Purpose Crew Vehicle (MPCV) is the first crew transport vehicle to be developed by the National Aeronautics and Space Administration (NASA) in the last thirty years. Orion is currently being developed to transport the crew safely beyond Earth orbit. This year, the vehicle focused on building the Exploration Flight Test 1 (EFT1) vehicle to be launched in 2014. The development of the Orion Environmental Control and Life Support (ECLS) System, focused on the completing the components which are on EFT1. Additional development work has been done to keep the remaining component progressing towards implementation for a flight tests in of EM1 in 2017 and in and EM2 in 2020. This paper covers the Orion ECLS development from April 2012 to April 2013.
    Keywords: Spacecraft Design, Testing and Performance
    Type: JSC-CN-27502 , ICES Conference; Jul 14, 2012 - Jul 18, 2012; Aspen, CO; United States
    Format: application/pdf
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
  • 2
    facet.materialart.
    Unknown
    Multi Purpose Crew Vehicle Environmental Control and Life Support Development Status (2011)
    In:  CASI
    Details
    Publication Date: 2019-07-19
    Description: The Orion Multi Purpose Crew Vehicle (MPCV) is the first crew transport vehicle to be developed by the National Aeronautics and Space Administration (NASA) in the last thirty years. Orion is currently being developed to transport the crew safely from the Earth beyond Earth orbit. This year, the vehicle focused on building the Orion Flight Test 1 (OFT1) vehicle to be launched in 2013. The development of the Orion Environmental Control and Life Support (ECLS) System, focused on the components which are on OFT1 which includes pressure control and active thermal control systems, is progressing through the design stage into manufacturing. Additional development work was done to keep the remaining component progressing towards implementation for a flight test in 2017. This paper covers the Orion ECLS development from April 2011 to April 2012.
    Keywords: Spacecraft Design, Testing and Performance
    Type: JSC-CN-25199 , 42nd International Conference on Environmental Systems (ICES); Jul 15, 2012 - Jul 19, 2012; San Diego, CA; United States
    Format: application/pdf
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
  • 3
    facet.materialart.
    Unknown
    Orion Multi-Purpose Crew Vehicle Active Thermal Control and Environmental Control and Life Support Development Status (2013)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: The Orion Multi-Purpose Crew Vehicle (MPCV) is the first crew transport vehicle to be developed by the National Aeronautics and Space Administration (NASA) in the last thirty years. Orion is currently being developed to transport the crew safely beyond Earth orbit. This year, the vehicle focused on building the Exploration Flight Test 1 (EFT1) vehicle to be launched in 2014. The development of the Orion Environmental Control and Life Support (ECLS) System, focused on the completing the components which are on EFT1. Additional development work has been done to keep the remaining component progressing towards implementation for a flight tests in of EM1 in 2017 and in and EM2 in 2020. This paper covers the Orion ECLS development from April 2012 to April 2013.
    Keywords: Spacecraft Design, Testing and Performance
    Type: JSC-CN-28786 , 43rd International Conference on Environmental Systems; Jul 14, 2013 - Jul 18, 2013; Vail, CO; United States
    Format: application/pdf
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
  • 4
    facet.materialart.
    Unknown
    Project Orion, Environmental Control and Life Support System Integrated Studies (2008)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: Orion is the next vehicle for human space travel. Humans will be sustained in space by the Orion subystem, environmental control and life support (ECLS). The ECLS concept at the subsystem level is outlined by function and technology. In the past two years, the interface definition with other subsystems has increased through different integrated studies. The paper presents the key requirements and discusses three recent studies (e.g., unpressurized cargo) along with the respective impacts on the ECLS design moving forward.
    Keywords: Spacecraft Design, Testing and Performance
    Type: SAE-08ICES-01-0198 , JSC-CN-15794 , International Conference on Environmental Sciences; Jun 30, 2008 - Jul 03, 2008; San Francisco, CA; United States
    Format: application/pdf
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
  • 5
    facet.materialart.
    Unknown
    Orion Multi Purpose Crew Vehicle Environmental Control and Life Support Development Status (2012)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: The Orion Multi Purpose Crew Vehicle (MPCV) is the first crew transport vehicle to be developed by the National Aeronautics and Space Administration (NASA) in the last thirty years. Orion is currently being developed to transport the crew safely from the Earth beyond Earth orbit. This year, the vehicle focused on building the Exploration Flight Test 1 (EFT1) vehicle to be launched in 2014. The development of the Orion Environmental Control and Life Support (ECLS) System, focused on the components which are on EFT1 which includes pressure control and active thermal control systems, is progressing through the design stage into manufacturing. Additional development work was done to keep the remaining component progressing towards implementation for a flight tests in 2017 and in 2020. This paper covers the Orion ECLS development from April 2011 to April 2012.
    Keywords: Spacecraft Design, Testing and Performance
    Type: JSC-CN-26159 , 42nd International Conference on Environmental Systems (ICES); Jul 15, 2012 - Jul 19, 2012; San Diego, CA; United States
    Format: application/pdf
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
  • 6
    facet.materialart.
    Unknown
    Extravehicular Mobility Unit (EMU) / International Space Station (ISS) Coolant Loop Failure and Recovery (2006)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: Following the Colombia accident, the Extravehicular Mobility Units (EMU) onboard ISS were unused for several months. Upon startup, the units experienced a failure in the coolant system. This failure resulted in the loss of Extravehicular Activity (EVA) capability from the US segment of ISS. With limited on-orbit evidence, a team of chemists, engineers, metallurgists, and microbiologists were able to identify the cause of the failure and develop recovery hardware and procedures. As a result of this work, the ISS crew regained the capability to perform EVAs from the US segment of the ISS.
    Keywords: Spacecraft Design, Testing and Performance
    Type: SAE-2006-01-2240 , ICES; Jul 16, 2006 - Jul 19, 2006; Norfolk, VA; United States
    Format: application/pdf
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
  • 7
    facet.materialart.
    Unknown
    Boeing Crew Exploration Vehicle Environmental Control and Life Support System Architecture Overview (2007)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: The Boeing Company under the teaming agreement with the Northrop Grumman Systems Corporation and in compliance with the NASA Phase 1 contract, had the responsibilities for the CEV architecture development of the Environmental control and life support (ECLS) system under the NASA Phase 1 contract. The ECLS system was comprised of the various subsystems which provided for a shirt-sleeve habitable environment for crew to live and work in the crew module of the CEV. This architecture met the NASA requirements to ferry cargo and crew to ISS, and Lunar sortie missions, with extensibility to long duration missions to Moon and MARS. This paper provides a summary overview of the CEV ECLS subsystems which was proposed in compliance with the contract activities.
    Keywords: Spacecraft Design, Testing and Performance
    Type: Rept-07ICES-284 , International Conference of Environmental Systems; Jul 09, 2007 - Jul 12, 2007; Chicago, IL; United States
    Format: text
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
  • 8
    facet.materialart.
    Unknown
    Crew Exploration Vehicle Environmental Control and Life Support Ddevelopment Status (2010)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: The Orion Crew Exploration Vehicle (CEV) is the first crew transport vehicle to be developed by the National Aeronautics and Space Administration (NASA) in the last thirty years. The CEV is being developed to transport the crew safely from the Earth to the Moon and back again. This year, the vehicle continued to go through design refinements to reduce weight, meet requirements, and operate reliably. Preliminary Design Review was performed and long lead procurement items were started. The design of the Orion Environmental Control and Life Support (ECLS) system, which includes the life support and active thermal control systems, is progressing through the design stage into manufacturing. This paper covers the Orion ECLS development from April 2009 to April 2010
    Keywords: Spacecraft Design, Testing and Performance
    Type: 2010-01-2457 , JSC-CN-20395 , ICES Meeting; Jul 11, 2010 - Jul 15, 2010; Barcelona; Spain
    Format: text
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
  • 9
    facet.materialart.
    Unknown
    International Space Station (ISS) Metal Oxide (MetOx) Odor Anomaly (2004)
    In:  Other Sources
    Details
    Publication Date: 2019-07-18
    Description: On occasion, seemingly normal operations can have significant effects upon the closed environment of the International Space Station (ISS). An example of such a case occurred on February 20, 2002 when a nominal Metal Oxide (MetOx) canister regeneration operation onboard the ISS resulted in an unexpected, foul odor that affected the crew and station operations. A case study summarizing the root cause for the event and steps taken to ensure that future MetOx regeneration operations proceed safely is presented. Included in the summary are engineering analyses and environmental monitoring results supporting the root cause assessment as well as testing conducted and flight operations changes implemented to ensure safe operations.
    Keywords: Spacecraft Design, Testing and Performance
    Type: International Conference on Environmental Systems (ICES); Jul 19, 2004 - Jul 22, 2004; Colorado Springs, CO; United States
    Format: text
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
  • 10
    facet.materialart.
    Unknown
    Orion Post Landing LiOH and Toxic Sensor Development (2010)
    In:  CASI
    Details
    Publication Date: 2019-07-19
    Description: The Orion Crew Exploration Vehicle (CEV) lands in the water with most resources depleted. There is a need to provide CO2 control while the cabin remains sealed for two hours post landing and there is a need to verify the outside air is free of ammonia or propellants, which may be venting from the vehicle, prior to opening the cabin. Development of approaches to perform these tasks while minimizing weight, volume, and cost are being investigated. This paper will document the results of those investigations.
    Keywords: Spacecraft Design, Testing and Performance
    Type: JSC-CN-22127 , International Conference on Environmental Systems (ICES); Jul 17, 2011 - Jul 21, 2011; Portland, OR; United States
    Format: application/pdf
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
Close ⊗
This website uses cookies and the analysis tool Matomo. More information can be found here...