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基本信息

AS42701
Validation Methods For MIL-STD-1760D Mission Stores
Validation Methods For MIL-STD-1760D Mission Stores
有效
【范围】 This document establishes techniques for validating that a mission store complies with the interface requirements contained in MIL-STD-1760 Revision D. 1.1 Purpose The purpose of this document is to provide methods for validating that a mission store’s electrical interface complies with the mission store interface (MSI) requirements of MIL-STD-1760. This document provides a set of modular, independent methods covering each of the requirements placed on the store by MIL-STD-1760. The methods contained herein apply to both the primary and auxiliary interfaces of MIL-STD-1760. 1.2 Application The methods herein apply to the initial validation of a store design to the requirements of MIL-STD-1760 and are expected to be conducted as part of store design validation as opposed to qualification test, conformance test, flight-line test, etc. The methods contained in this document are sufficient to encompass the Class I interface. Mission stores with Class II MSIs will use the appropriate subset of these Class I methods. 1.3 Tailoring The methods contained herein are general methods for conducting mission store validation and, as such, do not provide detailed procedures for these methods. It is intended that detailed procedures for validation of a specific mission store will be covered by tailored test plans and procedures prepared specifically for that store. These tailored test procedures would, for example, address those store-specific commands required to step through sufficient operations and states to demonstrate compliance with the particular aircraft/store electrical interconnection system (AEIS) requirement under test. 1.4 Limitations: The methods contained herein are based on MIL-STD-1760. This AS is based on the assumption that all tests are conducted at the store’s MSI connector and measurements of store performance occur only at this MSI connector. 1.5 Identification System: The test methods contained in this document are designated by an alphanumeric identification scheme. Each method is identified by a three alphabetical character combination followed by a three-digit number. The meaning of the first three characters is: a. HBW: High Bandwidth Interface b. MUX: Digital Multiplex Data Interface c. LBW: Low Bandwidth Interface d. REL: Release Consent Interface e. INL: Interlock Interface f. ADR: Address Interface g. GND: Structure Ground h. 28V: 28 V DC Power Interface i. ACP: 200 V AC Power Interface j. HDC: 270 V DC Power Interface k. FOC: Fiber Optic Interface l. INI: Initialization m. INT: Interrupts n. CON: MSI Connector o. COM: Communication Rules p. MSG: Messages on the Digital Multiplex Data Interface q. MDT: Mass Data Transfer r. GPS: GPS rf The three numbers following the letter code is a sequentially assigned number such that numbers 101 to 199 are for aircraft station interface (ASI) requirements and 201 to 299 are for mission stores interface (MSI) requirements. When applicable, the letter following this three-digit number is the test method revision letter. For example, HBW201 represents the original version of the first test requirement for the MSI high bandwidth interface while HBW201A represents the first revision of that test requirement.strRefField
【与前一版的变化】

包含缩略语

AC
ACP
ADR
AEIS
AS
ASD
ASI
AUX
BC
COM
CON
CSSI
dB
dBm
DC
DCP
FOC
GHz
GND
GPS
HB
HBW
HDBK
HDC
Hz
ICD
INI
INL
INT
kHz
LB
LBW
mA
MDT
MHz
MIL
ms
MSG
MSI
MUX
N/A
p-p
REL
RNASP
RT
RMS
SAE
STANAG
STD
TDP
TR
TRMS
UUT
V
VSWR

引用文件/被引文件

Production Test Plan for the Digital Time Division Command/Response Multiplex Data Bus Remote Terminals
Production Test Plan for the Digital Time Division Command/Response Multiplex Data Bus Controllers
Test Plan for the Digital Time Division Command/Response Multiplex Data Bus Couplers
Validation Methods for MIL-STD-1760 Mission Stores
Digital Time Division Command/Response Multiplex Data Bus
Aircraft Internal Time Division Command/Response Multiplex Data Bus
Multiplex Applications Handbook
Aircraft/Store Electrical Interconnection System Handbook
Aircraft/Store Electrical Interconnection System
General Specification For Connectors and Accessories
General Specification For Connectors
Insert Arrangements For MIL-C-38999 and MIL-C-27599 and MIL-C-29600 Electrical Circular Connectors
General Design Criteria for Airborne Stores
Measurement Management Systems - Requirements for Measurement Processes and Measuring Equipment
General Requirements For Calibration Laboratories & Measuring & Test Equipment
Analogue Video Standard for Aircraft System Applications
Navstar Global Positioning System (GPS) System Characteristics

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包含图表

HIGH BANDWIDTH VALID
HBW210: EQUIVALENT C
MISSION STORE DATA B
LOW BANDWIDTH VALIDA
LBW203
LBW204
LBW205
LBW206
LBW208
LBW209
RELEASE CONSENT INTE
REL204: TEST CONFIGU
INTERLOCK VALIDATION
202A: INTERLOCK CIRC
202B: INTERLOCK CIRC
INL203A: INTERLOCK C
INL203B: INTERLOCK C
ADDRESS VALIDATION M
formula 1
ADR205
ADR206 TEST CONDITIO
MISSION STORE STRUCT
GND202
MISSION STORE 28 V D
28V204
28V206
MISSION STORE 115/20
ACP204: TEST SETUP F
ACP206: TEST SETUP M
MISSION STORE 270 V
HDC204: TEST SETUP F
HDC206: TEST SETUP F
MISSION STORE FIBER
MISSION STORE INITIA
MISSION STORE POWER
MISSION STORE CONNEC
MISSION STORE DATA B
MISSION STORE MESSAG
MASS DATA TRANSFER (
MASS DATA TRANSFER (
Mass Data Transfer (
table 1
MISSION STORE GPS RF
GPS202: MEASUREMENT

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