Language:
    • Available Formats
    • Options
    • Availability
    • Priced From ( in USD )
    • Printed Edition
    • Ships in 1-2 business days
    • $52.00
    • Add to Cart
    • Printed Edition + PDF
    • Immediate download
    • $70.00
    • Add to Cart

Customers Who Bought This Also Bought

 

About This Item

 

Full Description

1.1 This test method is used to evaluate for explosive reactivity of various lubricants in the presence of aerospace alloys under high shear conditions.

1.2 The values stated in SI units are to be regarded as the standard. In cases where materials, products, or equipment are available in inch-pound units only, SI units are omitted.

1.3 This standard is used to measure and describe the response of materials, products, or assemblies to heat and flame under controlled conditions, but does not by itself incorporate all factors required for fire hazard or fire risk assessment of the materials, products, or assemblies under actual fire conditions.

1.4 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

 

Document History

  1. ASTM D3115-95(2014)

    👀currently
    viewing


    Standard Test Method for Explosive Reactivity of Lubricants with Aerospace Alloys Under High Shear (Withdrawn 2019)

    • Most Recent
  2. ASTM D3115-95(2009)


    Standard Test Method for Explosive Reactivity of Lubricants with Aerospace Alloys Under High Shear

    • Historical Version
  3. ASTM D3115-95(2005)


    Standard Test Method for Explosive Reactivity of Lubricants with Aerospace Alloys Under High Shear

    • Historical Version
  4. ASTM D3115-95(2000)


    Standard Test Method for Explosive Reactivity of Lubricants with Aerospace Alloys Under High Shear

    • Historical Version
  5. ASTM D3115-95


    Standard Test Method for Explosive Reactivity of Lubricants with Aerospace Alloys Under High Shear

    • Historical Version