6-MIL-PRF-27201D.pdf

MIL-PRF-27201D

07 February 2007

SUPERSEDING

METRIC

MIL-PRF-27201C

22 December 1995

PERFORMANCE SPECIFICATION

PROPELLANT, HYDROGEN

This specification is approved for use by all Departments and Agencies of the Department of Defense.

Comments, suggestions, or questions on this document should be addressed to HQ AFPET/AFTT, 2430 C Street, Bldg 70, Area B, Wright-Patterson AFB, OH 45433-7632 or e-mailed to AFPET.AFTT@wpafb.af.mil. Since contact information can change, you may want to verify the currency of this address information using the ASSIST Online database at http://assist.daps.dla.mil.

AMSC N/A FSC 9135

DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.

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1. SCOPE

1.1 Scope. This specification covers the requirements for two types of hydrogen.

1.2 Classification. The hydrogen will be of the following types as specified (see 6.2).

1.2.1 Types. The types of hydrogen are as follows:

Type I - Gaseous

Type II - Liquid

2. APPLICABLE DOCUMENTS

2.1 General. The documents listed in this section are specified in sections 3, 4, or 5 of this specification. This section does not include documents cited in other sections of this specification or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified requirements of documents cited in sections 3, 4, or 5 of this specification, whether or not they are listed.

2.2 Non-government publications. The following documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract. (see 6.2)

ASTM INTERNATIONAL

ASTM E 29 Standard Practice for Using Significant Digits in Test Data to Determine Conformance with Specifications

ASTM F 307 Standard Practice for Sampling Pressurized Gas for Gas Analysis

ASTM F 310 Standard Practice for Sampling Cryogenic Aerospace Fluids

(Copies of these documents are available online at http://www.astm.org or the American Society for Testing and Materials, 100 Barr Harbor Drive, West Conshohocken PA 19428-2959)

COMPRESSED GAS ASSOCIATION (CGA)

CGA G-5.3 Commodity Specification for Hydrogen

(Copies of this document are available online at http://www.cganet.com or from the Compressed Gas Association, Inc., 4221 Walney Road, 5th floor, Chantilly, VA 20151-2923)

2.3 Order of precedence. In the event of a conflict between the text of this document and the references cited herein (except for related specification sheets), the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.

3. REQUIREMENTS

3.1 Grade requirements. The purity and impurity concentrations shall conform to the limits of Table I when tested in accordance with the applicable test method also specified in Table I. Other limits and tests may be specified by the procuring activity (see 6.2).

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TABLE I. Limits for hydrogen.

Test Method

Purity, % by vol, min

Parahydrogen % by vol, min 1

99.995

95.0

4.4.2

4.4.1

Impurities, ppm by vol, max

Nitrogen, water vapor, and total hydrocarbons

Oxygen and argon

Helium

Carbon monoxide and carbon dioxide

9.0

1.0

39.0

1.0

4.4.2

4.4.2

4.4.2

4.4.2

4.4.2

Notes

1. Applies to Type II only.

3.2 Limiting values. The following applies to all specified limits in this specification: For purposes of determining conformance with these requirements, an observed value or a calculated value shall be rounded off "to the nearest unit" in the last right-hand digit used in expressing the specification limit according to the rounding-off method of ASTM E 29 Standard Practice for Using Significant Digits in Test Data to Determine Conformance with Specifications.

3.3 Filter. A filter with no more than a 10-micrometer nominal and 40-micrometer absolute rating shall be installed between the manufacturer's plant system and the manifold used to fill the gas or liquid containers for delivery.

3.4 Filled containers (Type I only).

3.4.1 Pressure. The container filling pressure shall not differ from that required by the contact by more than 1% at 70°F when tested as specified in 4.5.1. In no case shall the filling pressure exceed the rated service pressure of the container. The pressure-temperature table in section 6 may be used.

3.4.2 Leakage. Cylinders shall not leak when tested according to 4.5.2.

4. VERIFICATION

4.1 Points of inspection (see 6.2). Unless otherwise specified, acceptance tests shall be conducted at the site of filling prior to shipment or departure.

4.2 Conformance inspection. Quality conformance tests shall consist of the following:

a. Individual tests (Type I only)................................ 4.2.1

b. Sampling tests .................................................... 4.2.2

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c. In-stream test (Type II only) ................................ 4.2.3

4.2.1 Individual tests (Type I only). Each container shall be subjected to the following tests as described under 4.5:

a. Filling pressure .................................................... 4.5.1

b. Leakage .............................................................. 4.5.2

4.2.2 Sampling test. The number of hydrogen containers shall be selected in accordance with Table II and subjected to the tests required by Table I except for the parahydrogen test.

4.2.3 In-stream test. Liquid hydrogen shall be tested by an in-stream analyzer as described in 4.4.1.

TABLE II. Sampling for test.

Number of containers in lot Number of containers to be sampled

1 1

2 – 40 2

41 – 70 3

71 – over 4

4.2.4 Lot. A lot shall consist of one of the following:

a. Type I. For gas cylinders, a lot is defined as all of the hydrogen supplied in one or more container(s) filled from a single manifold at the same time. The first and last cylinders filled within a given lot are typically sampled. Other samples may be selected at random as required.

b. Type I. Gas containers that are interconnected by a single manifold that equalizes the pressure across all the containers shall be considered as one lot for the purpose of this specification.

c. Type II. Each filled container shall constitute a lot.

4.2.4.1 Sample. Each sample shall be of sufficient size to conduct all the quality conformance tests as specified herein. Unless otherwise specified, the quality conformance tests shall be performed on each required sample (see 6.2). When required, an equivalent sample shall be forwarded to a laboratory designated by the procuring activity for testing.

4.2.4.2 Sampling methods. Each sample taken for analysis shall be representative of the entire contents of the container being sampled. All apparatus used shall be made of suitable materials. Unless otherwise specified in the acquisition requirements (see 6.2), sampling shall be accomplished by one of the following methods.

a. Type I, gaseous hydrogen may be sampled in accordance with ASTM F 307 and Type II, liquid hydrogen may be sampled in accordance with ASTM F 310. It is critical that the sampling port be clean and free of contaminants.

b. Connect the shipping container being sampled directly to the analytical equipment using suitable pressure regulation as required to prevent over-pressurization of the equipment.

4.2.5 Non-bulk Containers. Non bulk containers are defined as containers with a water capacity of 400 liters, or less. The number of non-bulk containers Type I (gaseous) or Type II (liquid) hydrogen will be in accordance with Table II. Containers to be sampled may be selected at random.

4.2.6 Bulk Containers. Bulk containers are defined as having a water capacity in excess of 400 liters. Each bulk container filled with Type I (gaseous) and Type II (liquid) hydrogen constitutes a lot and shall be sampled.

4.2.6.1 Continuous service (see 6.4.1). Unless otherwise specified by the procuring activity, the following sample option for hydrogen shall be used for storage and transport tanks engaged in continuous hydrogen service (see 6.2). Contractor shall sample the contents of each transport tank engaged in continuous hydrogen service at least once every seven days at uniform intervals of time. Samples shall be taken from the filled transport tanks. Contractor shall sample the contents of each transport tank when entering continuous service and when the transport tank has remained empty for a period greater than 24 hours. When empty, all ports and vents shall remain closed to the atmosphere. While in continuous service, compliance with quality conformance tests specified herein shall be determined by sampling the filling point storage tank after each addition or, in case of continuous production, at established intervals not less frequent than once every 24 hours. When a storage tank is being filled during a change of duty shift, sampling shall be performed after filling.

4.3 Rejection. When any sample tested in accordance with 4.4 fails to conform to the requirements specified herein, the entire lot represented by the sample shall be rejected.

4.4 Analytical procedures. Unless otherwise specified, samples shall be analyzed according to the procedures described below (see 6.2). Calibration gas standards may be required to calibrate (zero and span) analytical instruments used to determine the purity and impurity contents of the hydrogen. The accuracy of the calibration gas standards is to be traceable to the National Institute of Standards and Technology (NIST).

4.4.1 Parahydrogen. Parahydrogen shall be determined by thermal conductivity type in-stream analyzers installed in the manufacturer's plant system. Analyzers shall be calibrated integrally by the appropriate use of temperature-controlled catalyst beds.

4.4.2 Gaseous purity and gaseous impurities. Methods shall be selected from those of

CGA G-5.3.

4.5 Containers of Type I hydrogen.

4.5.1 Filling pressure. Containers shall be tested for proper filling pressure by attaching a calibrated Bourdon-tube gauge or equivalent to the valve outlet and by attaching either a thermocouple or thermometer to the container wall. The gauge shall have scale divisions not greater than 100 kPa (15 psi). If a thermometer is used, tape or putty shall be applied to the bulb to protect it from extraneous temperatures. Putty shall not be applied between the bulb and the container wall. The thermometer shall have scale divisions not greater than 1°C (2°F). The container shall be stabilized to ambient temperature.

Then the valve shall be opened and the internal pressure observed on the gauge.

4.5.2 Leakage. Each Type I hydrogen container shall be tested for leaks at the neck threads, stem packing, and safety device of the valve with leak-detection fluid. Valve seat leakage shall be tested after filling has been completed. This shall be done by applying the leak-detection fluid sparingly across the outlet of the valve. Only leak-detection fluid that leaves no residue shall be used on the outlet.

5. PACKAGING

5.1 Packaging. For acquisition purposes, the packaging requirements shall be as specified in the contract or order (6.2). When packaging of materiel is to be performed by DoD or in-house contractor personnel, these personnel need to contact the responsible packaging activity to ascertain packaging requirements. Packaging requirements are maintained by the Inventory Control Point’s packaging activities within the Military Service or Defense Agency, or within the military service’s system commands.

Packaging data retrieval is available from the managing Military Department’s or Defense Agency’s automated packaging files, CD-ROM products, or by contacting the responsible packaging activity.

6. NOTES

(This section contains information of a general or explanatory nature that may be helpful, but is not mandatory.)

6.1 Intended use. The propellant covered by this specification is intended for use as a fuel in rocket engines and other space applications.

6.2 Acquisition requirements. Acquisition documents must specify the following:

a. Title, number, and date of this specification.

b. Type of hydrogen required (see 1.2).

c. When other limits or tests are required (see 3.1).

d. When a variation in the points of inspection is required (see 4.1).

e. When a variation of the quality conformance tests to be performed on a sample is required (see 4.2.4.1).

f. When a variation to the sampling method is required (see 4.2.4.2).

g. When a variation to the continuous service option is required (see 4.2.6.1).

h. When a variation of the analytical procedures is required (see 4.4).

i. Packaging requirements (see 5.1 and 6.3).

6.3 Packaging requirements. Guidance for cylinders may be found in the following documents:

a. RR-C-901 Cylinders, Compressed Gas: Seamless Shatterproof, High Pressure DOT 3AA Steel, and 3AL Aluminum

b. MIL-DTL-2/29 Valve, Cylinder, Gas, Hydrogen Outlet 350

c. MIL-STD-101 Color Code for Pipelines and for Compressed Gas Cylinders

d. MIL-STD-1411 Inspection and Maintenance of Compressed Gas Cylinders

e. 49 CFR 171 – 199 Code of Federal Regulations

6.4 Definitions.

6.4.1 Continuous service. Continuous service applies to continuous deliveries under Government contract of hydrogen complying with the quality conformance tests specified herein.

6.4.2 In-stream analyzer. An analyzer with its sensor in the product stream or which receives samples directly from the product stream.

6.5 Part or identifying number. The PINs to be used for hydrogen acquired to this specification are created as follows:

M 27201 - X Example of PIN: M27201-2

Type (see 1.2.1). Use 1 for Type I, 2 for Type II.

Specification number.

Prefix for military specification.

6.6 Subject term (key word) listing.

Aerospace Cryogenic Cylinders Hydrogen Propellant Rocket engines

6.7 Changes from previous issue. Marginal notations are not used in this revision to identify changes with respect to the previous issue due to the extent of the changes.

6.8 Temperature-pressure relation. Table III has been derived using the values of NBS (now NIST) Technical Note 1079 and the relations for thermal expansion and cylinder stretch of Bureau of Mines publication IC 8367.

TABLE III. Pressure-temperature conversion.

Service pressure (psig) Temperature

(°F) 1800 2000 2015 2200 2265 2400 -40 1419 1576 1587 1733 1783 1889 -38 1426 1583 1594 1741 1792 1898 -36 1433 1591 1602 1750 1801 1908 -34 1440 1599 1610 1758 1809 1917 -32 1447 1606 1618 1767 1818 1926 -30 1454 1614 1626 1775 1827 1936 -28 1461 1622 1633 1784 1836 1945 -26 1468 1630 1641 1792 1844 1954 -24 1474 1637 1649 1801 1853 1963 -22 1481 1645 1657 1809 1862 1973 -20 1488 1653 1665 1818 1871 1982 -18 1495 1660 1672 1826 1879 1991 -16 1502 1668 1680 1835 1888 2001 -14 1509 1676 1688 1843 1897 2010 -12 1516 1684 1696 1852 1906 2019 -10 1523 1691 1703 1860 1914 2028 -8 1530 1699 1711 1869 1923 2038 -6 1537 1707 1719 1877 1932 2047 -4 1544 1714 1727 1886 1941 2056 -2 1551 1722 1735 1894 1949 2066 0 1557 1730 1742 1903 1958 2075 2 1564 1738 1750 1911 1967 2084 4 1571 1745 1758 1920 1976 2093 6 1578 1753 1766 1928 1985 2103 8 1585 1761 1774 1937 1993 2112 10 1592 1768 1781 1945 2002 2121 12 1599 1776 1789 1954 2011 2131 14 1606 1784 1797 1962 2020 2140 16 1613 1792 1805 1971 2028 2149 18 1620 1799 1813 1979 2037 2159 20 1627 1807 1820 1988 2046 2168 22 1634 1815 1828 1996 2055 2177 04 1640 1822 1836 2005 2063 2186 26 1647 1830 1844 2013 2072 2196 28 1654 1838 1851 2022 2081 2205 30 1661 1846 1859 2030 2090 2214 32 1668 1853 1867 2039 2098 2224 34 1675 1861 1875 2047 2107 2233 36 1682 1869 1883 2056 2116 2242 38 1689 1876 1890 2064 2125 2251 40 1696 1884 1898 2072 2134 2261 42 1703 1892 1906 2081 2142 2270 44 1710 1900 1914 2089 2151 2279

TABLE III. Pressure-temperature conversion - Continued.

Service pressure (psig) Temperature

(°F) 1800 2000 2015 2200 2265 2400 46 1717 1907 1922 2098 2160 2289 48 1723 1915 1929 2106 2169 2298 50 1730 1923 1937 2115 2177 2307 52 1737 1930 1945 2123 2186 2316 54 1744 1938 1953 2132 2195 2326 56 1751 1946 1961 2140 2204 2335 58 1758 1954 1968 2149 2212 2344 60 1765 1961 1976 2157 2221 2354 62 1772 1969 1984 2166 2230 2363 64 1779 1977 1992 2174 2239 2372 66 1786 1984 1999 2183 2247 2381 68 1793 1992 2007 2191 2256 2391 70 1800 2000 2015 2200 2265 2400 72 1806 2008 2023 2208 2274 2409 74 1813 2015 2031 2217 2283 2419 76 1820 2023 2038 2225 2291 2428 78 1827 2031 2046 2234 2300 2437 80 1834 2038 2054 2242 2309 2447 82 1841 2046 2062 2251 2318 2456 84 1848 2054 2070 2259 2326 2465 86 1855 2062 2077 2268 2335 2474 88 1862 2069 2085 2276 2344 2484 90 1869 2077 2093 2285 2353 2493 92 1876 2085 2101 2293 2361 2502 94 1883 2092 2108 2302 2370 2512 96 1889 2100 2116 2310 2379 2521 98 1896 2108 2124 2319 2388 2530

100 1903 2116 2132 2327 2396 2539 102 1910 2123 2140 2336 2405 2549 104 1917 2131 2147 2344 2414 2558 106 1924 2139 2155 2353 2423 2567 108 1931 2146 2163 2361 2432 2577 110 1938 2154 2171 2370 2440 2586 112 1945 2162 2179 2378 2449 2595 114 1952 2170 2186 2387 2458 2604 116 1959 2177 2194 2395 2467 2614 118 1966 2185 2202 2404 2475 2623 120 1972 2193 2210 2412 2484 2632 122 1979 2200 2218 2421 2493 2642 124 1986 2208 2225 2429 2502 2651 126 1993 2216 2233 2438 2510 2660 128 2000 2224 2241 2446 2519 2670 130 2007 2231 2249 2455 2528 2679

CONCLUDING MATERIAL

Custodians: Preparing activity:

Army – MI Air Force – 68 Navy – AS (Project 9135-2005-006) Air Force – 68

DLA – PS

Review activities:

Air Force – 19

Civil Agency:

NASA – NA

Note: The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information using the ASSIST Online database at http://assist.daps.dla.mil.

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