MIL-DTL-85097/1B(OS)
AS 3554
Propellant, N-44(U)
(Application for copies should be addressed to Commander, Naval Air Systems Command, Code 51122E,
Washington, DC 20361.)
DRAWINGS
NAVAL AIR SYSTEMS COMMAND (CAGE Code 30003)
707AS129
Container Assembly, for Rocket Catapults
707AS130
Palletization Assembly, Rocket Catapults
707AS300
Assembly, Rocket Catapult, MK 16 Mod 1
707AS190
Test Chamber
707AS191
Test Setup Assembly
707AS192
Adapter
(Application for copies should be addressed to the Commander, Indian Head Division, Naval Surface
Warfare Center, Attn: Code 8410P, 101 Strauss Avenue, Indian Head, MD 20640-5035.)
PUBLICATIONS
NAVAL SEA SYSTEMS COMMAND
OP 2165
Navy Transportation Safety Handbook for Hazardous Materials
(Application for copies should be addressed to the Commanding Officer, Naval Publications and Forms
Center, Attn: 1053, 5801 Tabor Avenue, Philadelphia, PA 19120-5099.)
2.3 Order of precedence. In the event of a conflict between the text of this document and the references
cited herein, 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 General. The requirements in this specification sheet, unless in direct conflict with the basic
specification, shall be considered additional, not substitute. The loaded rocket catapult shall conform to the
documents specified herein and to Drawing 736AS300.
3.2 Preproduction.
3.2.1 Propellant aging. When tested in accordance with MIL-DTL-85097, the cartridge and sustainer
propellants shall meet the requirements of table I or table II, as applicable.
3.2.2 Load. The rocket catapult shall withstand a static compression load of 18,000 pounds and a tension
load of 8,700 pounds applied along the longitudinal axis at the attachment points without failure.
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