MIL-C-26482, Series 2 Connectors
PV
• Intermatable with MIL-C-26482 Series I
• Operating termperature - 55˚C to + 200˚C
The PV connector is designed to meet the rugged
requirements of MIL-C-26482, Series 2/MIL-C-83723
Series I*, the specification which delineates
the critical requirements of space-age applications. PV
connectors have been used extensively on major
aerospace programs requiring general-purpose,
miniature cylindrical bayonet coupling connectors
such as Space Shuttle, Apollo, ATM, OWS Min-
uteman, Skylab, Thor-Delta, Titan IIIC, and Viking.
4
1
3
The PV series is an important member of the
Universal Interconnect System (UIS)
- the only
system that can perform all interconnection mis-
sions. This system is adaptable for use with connec-
tors of all shapes and sizes, including circular and
rectangular configurations. standard, miniature and
subminiature sizes. UIS is a rear servicing system
that evolved from the LITTLE CAESAR® rear re-
lease contact retention assembly, pioneered and
developed by ITT Cannon. Since this time,
ITT Cannon, and its licensees, have supplied to
industry over 250 million interconnections utilizing
this system.
2
Universal Insertion
/ Extraction Tool Style - A
single,expendable plastic tool is used for insertion and
extraction of both pins and sockets.
Simple, Strong Contact Design - One basic config-
uration eliminates undercuts and maximizes bend re-
sistance for positive contact mating.
Closed-Entry Socket Insert
face of mating connector has lead-in chamfers for
positive alignment of pins and sockets.
- Hard dielectric socket
PV7 connectors are available under numerous in-
dustrial specifications, some of which are listed
below:
• CS512089 Jet Propulsion Laboratory
• 40M39569 NASA, George C. Marshall Space
Flight Center
• 81D52 Martin Marietta, Denver Division
• MG414-0365 Rockwell International Space
Division
Interfacial Pin Insert Seal
- Universal interconnect
permits design of raised moisture barriers around each
pin which mate into lead-in chambers of hard face
sockets insert for individual contact sealing. Interfacial
sealing is never touched by service tools.
Superior Contact Stability
- Rear Contact Release
• AC414-0013 Rockwell International Autonetics
Division
• STS0003 McDonnell Douglas Astronautics
System (LITTLE CAESAR contact assembly) features a
stamped metal retaining clip captivated by molded-in
shoulders of each contact cavity in the insulator. A
rear-inserted plastic tool expands the tines beyond the
contact shoulder, releasing the contact.
This connector series is manufactured to accommo-
date the following backshells: M85049/31
(MS3416), M85049/51 (MS3418) and M85049/
52 (MS3417). Backshells are not included with
connector and must be ordered separately. Back-
shells on page 161 are Non-MS type.
Polarized Backshells - Interlocking teeth on the front of the
backshell and rear portion of the shell allow
endbells to be positioned as desired, eliminating chaf-
ing of wire during assembly.
Military Specification Cross Reference
ITT Cannon Prefix
PV7 and MIL-C-26482
(Series 2) Replacement for
MS Standards
MIL-C-83723*
Slash Sheet
Commercial
Design
Description
MIL-C-26482 (Series 1)
MIL-C-26482
PV70
PV71
PV70
PV74
PV76
PV72
PV75
Socket
Pin
MS3110,MS3120
MS3111,MS3121
MS3112,MS3122
MS3114,MS3124
MS3116,MS3126
MS3470
MS3471
MS3470
MS3474
MS3476
MS3472
MS3475
/1
/7
/1
/5
/13
/3
/43
/2
/8
/12
/6
/14
/4
Narrow Flange Receptacle
Cable Connecting Receptacle
Narrow Flange Receptacle
Jam Nut Receptacle
Straight Plug
Wide Flange Receptacle
Straight Plug, RFI Shielded
/42
NAS1599
NAS1650,NAS1699
NAS1651,NAS1700
NAS1652,NAS1701
NAS1653,NAS1702
MS3470
MS3472
MS3474
MS3476
/1
/3
/5
/13
/2
/4
/6
/14
Narrow Flange Receptacle
Wide Flange Receptacle
Jam Nut Receptacle
Straight Plug
*NOTE: M83723 series has been superseded by MIL-C-26482 Series 2.
Dimensions are shown in inches (millimeters).
Dimensions subject to change.
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