Refine Your Search

Search Results

Standard

Methods for Evaluating Cryogenic Filters

2017-08-15
WIP
ARP900C
The purpose of this test procedure is to present test methods that can be utilized to evaluate the filtration and operating characteristics of filters that will be utilized in a cryogenic system. The methods presented herein are intended to supplement standard filter testing specifications to allow evaluation of filter performance characteristics in areas that could be affected by extreme low temperatures. The test methods can be utilized to evaluate filters up to and including 60 gpm (230 lpm) capacity. If higher flow rate filters are to be evaluated in accordance with the test methods presented herein, it will be necessary to increase the system flow capacity and the size of effluent sampling system. The test methods presented herein do not encompass testing of cryogenic bypass relief valves, delta P indicators, gages, or components other than a basic filter housing and element.
Standard

Methods for Evaluating Cryogenic Filters

2011-12-19
CURRENT
ARP900B
The purpose of this document is to present test methods that can be utilized to evaluate the filtration and operating characteristics of filters that will be utilized in a cryogenic system. The methods presented herein are intended to supplement standard filter testing specifications to allow evaluation of filter performance characteristics in areas that could be affected by extreme low temperatures. The test methods can be utilized to evaluate filters for particle sizes equal to or greater than 5.0 μm and flows up to and including 60 gpm (230 L/min) capacity. If higher flow rate filters are to be evaluated in accordance with the test methods presented herein, it will be necessary to increase the system flow capacity and the size of effluent sampling system from those recommended in this document.
Standard

Methods for Evaluating Cryogenic Filters

1992-06-29
HISTORICAL
ARP900A
The purpose of this test procedure is to present test methods that can be utilized to evaluate the filtration and operating characteristics of filters that will be utilized in a cryogenic system. The methods presented herein are intended to supplement standard filter testing specifications to allow evaluation of filter performance characteristics in areas that could be affected by extreme low temperatures. The test methods can be utilized to evaluate filters up to and including 60 gpm (230 lpm) capacity. If higher flow rate filters are to be evaluated in accordance with the test methods presented herein, it will be necessary to increase the system flow capacity and the size of effluent sampling system.
Standard

Steel Tubing, Seamless, 0.50ni 0.55cr 0.20mo (0.28 0.33c)

1943-10-01
HISTORICAL
AMS6530A
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of February 1995. The requirements of this specification are embodied in the laths issue of AMS 6360.
Standard

Steel Tubing, Seamless, 0.50ni 0.55cr 0.20mo (0.28 0.33c)

1942-09-01
HISTORICAL
AMS6530
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of February 1995. The requirements of this specification are embodied in the laths issue of AMS 6360.
Standard

Steel Tubing, Seamless, 0.50ni 0.55cr 0.20mo (0.28 0.33c)

1982-04-01
HISTORICAL
AMS6530G
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of February 1995. The requirements of this specification are embodied in the laths issue of AMS 6360.
Standard

Steel Tubing, Seamless, 0.50ni 0.55cr 0.20mo (0.28 0.33c)

1975-06-15
HISTORICAL
AMS6530F
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of February 1995. The requirements of this specification are embodied in the laths issue of AMS 6360.
Standard

Steel Tubing, Seamless, 0.50ni 0.55cr 0.20mo (0.28 0.33c)

1988-10-01
HISTORICAL
AMS6530H
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of February 1995. The requirements of this specification are embodied in the laths issue of AMS 6360.
Standard

Steel Tubing, Seamless, 0.50ni 0.55cr 0.20mo (0.28 0.33c)

1950-12-01
HISTORICAL
AMS6530C
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of February 1995. The requirements of this specification are embodied in the laths issue of AMS 6360.
Standard

Steel Tubing, Seamless, 0.50ni 0.55cr 0.20mo (0.28 0.33c)

1945-07-01
HISTORICAL
AMS6530B
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of February 1995. The requirements of this specification are embodied in the laths issue of AMS 6360.
Standard

Steel Tubing, Seamless, 0.50ni 0.55cr 0.20mo (0.28 0.33c)

1969-05-01
HISTORICAL
AMS6530E
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of February 1995. The requirements of this specification are embodied in the laths issue of AMS 6360.
Standard

Steel Tubing, Seamless, 0.50ni 0.55cr 0.20mo (0.28 0.33c)

1953-02-15
HISTORICAL
AMS6530D
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of February 1995. The requirements of this specification are embodied in the laths issue of AMS 6360.
Standard

Steel Tubing, Seamless, 0.50cr 0.55ni 0.20mo (0.28 0.33c)

1942-09-01
HISTORICAL
AMS6535
Primarily for use where welding and moderate tensile properties are required. May be used where minimum tensile strength up to 180,000 psi (1240 MPa) is required for wall thicknesses up to 0.125 in. (3 mm) and proportionately lower strength is required in heavier thicknesses. This specification has been declared "Noncurrent" by the Aerospace Materials Division, SAE, as of 19 April 1988. It is recommended, therefore, that this specification not be specified for new designs.
Standard

Steel Tubing, Seamless, 0.50cr 0.55ni 0.20mo (0.28 0.33c)

1950-12-01
HISTORICAL
AMS6535C
Primarily for use where welding and moderate tensile properties are required. May be used where minimum tensile strength up to 180,000 psi (1240 MPa) is required for wall thicknesses up to 0.125 in. (3 mm) and proportionately lower strength is required in heavier thicknesses. This specification has been declared "Noncurrent" by the Aerospace Materials Division, SAE, as of 19 April 1988. It is recommended, therefore, that this specification not be specified for new designs.
X