Explore: Cold Flow Tests

Discover books, insights, and more — all in one place.

Learn more about Cold Flow Tests with top reads curated from trusted sources — all in one place.

Topic Search

Search for any topic

AI-Generated Overview About “cold-flow-tests”:


Books Results

Source: The Open Library

The Open Library Search Results

Search results from The Open Library

1Simulation of cold-test parameters and RF output power for a coupled-cavity traveling-wave tube

By

“Simulation of cold-test parameters and RF output power for a coupled-cavity traveling-wave tube” Metadata:

  • Title: ➤  Simulation of cold-test parameters and RF output power for a coupled-cavity traveling-wave tube
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  Springfield, Va - [Washington, D.C

“Simulation of cold-test parameters and RF output power for a coupled-cavity traveling-wave tube” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1995
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

Online Access

Downloads Are Not Available:

The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

Online Borrowing:

    Online Marketplaces

    Find Simulation of cold-test parameters and RF output power for a coupled-cavity traveling-wave tube at online marketplaces:


    2Development of an empirical method for predicting jet mixing noise of cold flow rectangular jets

    By

    “Development of an empirical method for predicting jet mixing noise of cold flow rectangular jets” Metadata:

    • Title: ➤  Development of an empirical method for predicting jet mixing noise of cold flow rectangular jets
    • Author:
    • Language: English
    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
    • Publish Date:
    • Publish Location: Hampton, Va - Springfield, VA

    “Development of an empirical method for predicting jet mixing noise of cold flow rectangular jets” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1999
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Access

    Downloads Are Not Available:

    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

    Online Borrowing:

      Online Marketplaces

      Find Development of an empirical method for predicting jet mixing noise of cold flow rectangular jets at online marketplaces:


      3Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream

      By

      “Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream” Metadata:

      • Title: ➤  Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream
      • Author:
      • Language: English
      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
      • Publish Date:
      • Publish Location: ➤  [Washington, DC] - [Springfield, Va

      “Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1995
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: No_ebook

      Online Access

      Downloads Are Not Available:

      The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

      Online Borrowing:

        Online Marketplaces

        Find Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream at online marketplaces:


        4Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations

        By

        “Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations” Metadata:

        • Title: ➤  Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations
        • Author:
        • Language: English
        • Publisher: ➤  Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
        • Publish Date:
        • Publish Location: ➤  [Cleveland, Ohio] - Hanover, MD

        “Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 2001
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

        Online Access

        Downloads Are Not Available:

        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

        Online Borrowing:

          Online Marketplaces

          Find Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations at online marketplaces:



          Wiki

          Source: Wikipedia

          Wikipedia Results

          Search Results from Wikipedia

          Kuwait Space Rocket

          that flows around the nozzle and back into the injector again. The KSR team performed a cold flow testing in October 2019 to verify the engine's flow rate

          Linear Aerospike SR-71 Experiment

          hot-fire flight test because of liquid oxygen leaks in the test apparatus. The ground firings and the airborne cryogenic gas flow tests provided enough

          Pintle injector

          rocket engine. Like any other injector, its purpose is to ensure appropriate flow rate and intermixing of the propellants as they are forcibly injected under

          RP-1

          engines must be ground-fired some number of times before launch. Even cold-flow tests, in which the propellants are not ignited, can leave residues. On the

          NERVA

          full power. A subsequent full-power Kiwi B4A test on 30 November 1962, along with a series of cold flow tests, revealed that the problem was vibrations that

          ISRO

          and hence the engine needs very little refurbishment. The LPSC began cold flow tests of engine prototypes in 2020. ISRO's current launch vehicles lack the

          Spirometry

          common of the pulmonary function tests (PFTs). It measures lung function, specifically the amount (volume) and/or speed (flow) of air that can be inhaled and

          Raynaud syndrome

          pallor) and becomes cold and numb. These events are episodic, and when the episode subsides or the area is warmed, the blood flow returns and the skin

          Pyroclastic flow

          turbulence between the flow and the overlying air, admixing and heating cold atmospheric air causing expansion and convection. Flows can deposit less than

          Demonstration Rocket for Agile Cislunar Operations

          will be evaluated in a cold-flow test with a nonnuclear engine mock-up to assess the mechanical integrity of the core. Such tests were conducted during