MODEL NO. | SERIES LETTER | CUSTOMER | TYPE DESIGNATION | DESCRIPTION | DATE NO. ASSIGNED | JOB NUMBER |
85 | (BENDIX JS-2001B) | NAVY | MISSILE
(TALOS) | SURFACE-TO-AIR MISSILE, IMPROVED VERSION OF RTV-N-6A4, ADDITION OF WARHEAD AND FUSE, NEW COMBUSTOR, X BAND INTELLIGENCE (NOW X SAM-N-6) MODEL T [RAMJET] M1=1.76
SC A1 = 205 | 3 - 51
(EST.) | 09
18 |
85 |
A
(BENDIX JS -2001B) | NAVY | MISSILE
(TALOS 6A) | SURFACE-TO-AIR MISSILE SAME AS MODEL 85 EXCEPT C-BAND INTELLIGENCE (NOW X SAM-N-6A)
MODEL T [RAMJET] M1=1.76
SC A1 = 205 | 9 - 51
(EST.) | 09
18 |
85 | B
(BPD
4524) | NAVY | MISSILE
(TALOS 6B) | SURFACE-TO-AIR MISSILE , SIMILAR TO MODEL 85A WITH MODIFICATIONS TO THE DIFFUSER INLET, INNER BODY, FUZE, WARHEAD, WING ACTUATORS, COMBUSTOR AND BOOSTER; AND WITH A STIFFENED BODY. C-BAND INTELLIGENCE. (NOW X SAM-N-6B)
MODEL J -2 [RAMJET] F1 = 2.2
SC A1 = 235 | 11 - 52
(EST.) | 31
34
40 |
85 | B
(BPD
4524) | NAVY | MISSILE
(TALOS 6C) | SURFACE-TO-AIR MISSILE, SAME AS MODEL 85B WITH ELIMINATION OF PREVIOUSLY ALLOWED SPECIFICATION DEVIATION TO IMPROVE TACTICAL SUITABILITY. C-BAND INTELLIGENCE, (NOW X SAM-N-6B)
MODEL J-2 [RAMJET] M1 = 2.2
SC A1 = 235 | 11 - 52
(EST.) | NONE |
85 | D
(BPD 4271) | NAVY | MISSILE
(TALOS 6BW) | SURFACE-TO-AIR MISSILE, SAME AS MODEL 85B AFT OF STATION 105 WITH MINOR REFINEMENTS FORWARD OF STATION 105 AS COMPARED TO MODELS 85W AND 85SW. REFINEMENTS INCLUDE: INNER BODY REDESIGNED TO ACCOMMODATE A NEW DESIGN OF INNER-BODY CENTER SECTION, , ELIMINATION OF S & A BRACKETRY, AND NEW S & A PLUG. C-BAND INTELLIGENCE (NOW SAM- N-6BW)
MODEL J-2 [RAMJET] F1 = 2.2
SC A1 = 225 | 9-7-56 | 31
34
40 |
85 | E
(BPD
4271) | NAVY | MISSILE
(TALOS 6BW) | SURFACE-TO-AIR MISSILE, SAME AS MODEL 85B WITH REFINEMENTS FORWARD OF STATION 105 THAT INCLUDE REDESIGNED INNER BODY TO ACCOMMODATE A NEW DESIGN OF INNER BODY. C-BAND INTELLIGENCE (NOW X SAM-N-6BW)
MODEL J-2 [RAMJET] M1 = 2.2
SC A1 = 225 | 9-7-56 | 31
34
40 |
85 | F
(BPD 4271) | NAVY | MISSILE
(TALOS L) | SURFACE-TO-AIR MISSILE , L PROTOTYPE, REVISED DIFFUSER INLET, REPACKAGED FLUSH AND FORWARD ANTENNAS, LONGER FUEL TANK AND TAIL PIPE. INCREASED SPAN OF MISSILE FINS , ALTITUDE - BIASED, MACH NUMBER SPEED CONTROL, C-BAND INTELLIGENCE, (NOW X SAM -N-6B1)
MODEL J-2L [RAMJET] M1 = 2.73
SC A1 = 330 | 9-7-56 | 34
43 |
85 | G
(BPD 4402) | NAVY | MISSILE
(TALOS LW) | SURFACE-TO-AIR MISSILE , LW PROTOTYPE, REVISED DIFFUSER INLET, LONGER FUEL TANK AND TAILPIPE. INCREASED SPAN OF MISSILE FINS. ALTITUDE - BIASED, MACH NUMBER SPEED CONTROL, NEW INNER BODY
FORWARD SECTION. DOUBLE CONE INLET FOR LAST TWO SETS OF MCDONNELL PARTS IN ADDITION TO SINGLE CONE INLET PARTS. C-BAND INTELLIGENCE
(NOW X SAM-N-6BW1)
MODEL J-2L [RAMJET] M1 = 2.73
SC A1 = 330 | 9-7-56 | 34
43 |
85 | H
(BPD
4549
4599
4177A
4254
4813) | NAVY | MISSILE
(TALOS 6B) | SURFACE-TO-AIR MISSILE, IN-LINE CONFIGURATION OF MODEL 85B, PROVISION FOR WING CONTROL DURING BOOST, STOWAGE STRONG POINT AT B.S. 105, WAVEGUIDE INSTALLATION, C-BAND INTELLIGENCE
(NOW X SAM -N-6B)
MODEL J-2 [RAMJET] M1 = 2 .2
SC A1 = 225 | | 49
85
97 |
85 | J
(BPD
4550
4600
4271
4280
4813
4814 ) | NAVY | MISSILE
{TALOS 6BW) | SURFACE-TO-AIR MISSILE , IN-LINE CONFIGURATION OF MODEL 85D, PROVISION FOR WING CONTROL DURING BOOST, STOWAGE STRONG POINT AT B.S. 105 , WAVEGUIDE INSTALLATION, C-BAND INTELLIGENCE
(NOW X SAM-N-6BW)
MODEL J-2 [RAMJET] M1 = 2 .2
SC A1 = 225 | | 49
85
97 |
85 | K
(BPD
4402) | NAVY | MISSILE
(TALOS 6BW1) | SURFACE-TO-AIR MISSILE , DOUBLE CONE INLET VERSION OF MDDEL 85G, C-BAND INTELLIGENCE, (NOW X SAM-N-6BW1)
MODEL J-2L [RAMJET] M1 = 2 .73
DC A1 = 360 | 9-7-56 | 25
43 |
85 | L
(BENDIX
4401
4663) | NAVY | MISSILE
(TALOS 6B1) | SURFACE-TO-AIR MISSILE, IN-LINE CONFIGURATION OF MDDEL 85F , STOWAGE STRONG POINT AT B .S . 105 , MODULAR ELECTRONIC PACKAGING, MODIFIED SINGLE CONE INLET, WING CONTROL DURING BOOST, C-BAND INTELLIGENCE,
(NOW X SAM-N-6B1)
MODEL J-2L [RAMJET] M1 =3.1
SC A1 = 330 | 9-7-56 | 97 |
85 | M
(BPD
4402
4663
4401) | NAVY | MISSILE
(TALOS 6BW1) | SURFACE-TO-AIR MISSILE, IN-LINE CONFIGURATION OF MODEL 85G , STOWAGE STRONG POINT AT B .S . 105 , MODULAR ELECTRONIC PACKAGING, C-BAND INTELLIGENCE, (NCW X SAM-N-6BW1)
MODEL J-2L [RAMJET] M1= 2 .73
SC A1 = 360 | 9-7-56 | 97 |
85 | N
(BPD
4401
4663) | NAVY | MISSILE
(TALOS 6B1 - UNITIZED) | SURFACE-TO-AIR MISSILE, SAME AS MDDEL 85L EXCEPT FOR MOUNTING PROVISIONS AFT OF B .S . 105 FOR UNITIZED PACKAGING. (NOW X SAM-N-6B1)
MODEL J-2L [RAMJET] M1 = 3.1
SC A1 = 330 | 9-7-56 | 97
11
15 |
85 | P
(BPD
4402
4663
4401) | NAVY | MISSILE
(TALOS 6BW1 -
UNITIZED) | SURFACE-TO-AIR MISSILE, SAME AS MODEL 85M EXCEPT FOR MOUNTING PROVISIONS AFT OF B .S . 105 FOR UNITIZED PACKAGING. (NOW X SAM-N-6BW)
MODEL J - 2L [RAMJET] M1 = 2 .73
SC A1 = 360 | 9-7-56 | 97
11
15 |
85 | Q
(BPD
4401
4867 ) | NAVY | MISSILE
(TALOS 6B1 -
UNITIZED) | SURFACE-TO-AIR MISSILE, SAME AS MODEL 85N EXCEPT FOR PROVISIONS FOR DOUBLE CONE INLET (PREPRODUCTION PROTOTYPE) (NOW X SAM -N-6B1)
MODEL J - 2L M1 = 2 .73
SC A1 = 360 | 9-7-56 | 43
97 |
85 | R
(BPD
4852
4854) | NAVY | MISSILE
(TALOS 6B1) | SURFACE-TO-AIR MISSILE , HIGH PRODUCTION TALOS, SPUN DIFFUSERS CASTINGS USED. C-BAND INTELLIGENCE, (NOW X SAM -N-6B1)
MODEL J-2L [RAMJET] M1 = 2.73 DC | 9-7-56 | (MED)
NOT YET
ASSIGNED |
85 | S
(BENDIX
JS-2001B) | NAVY | MISSILE
(TALOS 6A) | SURFACE-TO-AIR MISSILE, SAME AS MODEL 85A EXCEPT FOR CONTRACT ARRANGEMENT AND REVISED BOOSTER FIN . C-BAND INTELLIGENCE. (NOW X SAM-N-6A)
MODEL T [RAMJET] M1 = 1.76
SC A1 = 205 | 8-53
(EST.) | (MED)
01-33
09
33 |
85 | SW
(APL
PLT-265 AS MOD. BY BPD
4217) | NAVY | MISSILE
(TALOS 6AW) | SURFACE-TO-AIR MISSILE, SAME AS MODEL 85W EXCEPT FOR QUICKLY REMOVABLE INNER BODY FORWARD CONE AND ELIMINATION OF ANGLE-OF-ATTACK PROBE. C-BAND INTELLIGENCE, (NOW X SAM-N-6AW)
MODEL T [RAMJET] M1 = 2 .2
SC A1 = 225 | 8-53
(EST.) | (MED)
01-33
33 |
85 | T
(BPD
4661
4854) | NAVY | MISSILE
(TALOS 6BW) | SURFACE-TO-AIR MISSILE. HIGH PRODUCTION TALOS, HYDRO-SPUN COWL, SPUN INNER BODY NOSE AND AFT CONE. C-BAND INTELLIGENCE. (NOW X SAM-N-6BW)
MODEL J-2L [RAMJET] M1 = 2 .73
DC A1 = 360 | 9-7-56 | (MED)
NOT YET
ASSIGNED |
85 | U
(BPD
4870) | NAVY | MISSILE
(TALOS 6BWLA -
UNITIZED) | SURFACE-TO-AIR MISSILE. HOMING VERSION OF MODEL 8 5J (6BW), UNITIZED AFT SECTION, MODULAR EIECTRONIC PACKAGING, PROVISIONS FOR STAPFUS, PROVISION FOR CONTACT FUSE, C-BAND INTELLIGENCE.
MODEL J-2L [RAMJET] M1 = 2.73
DC A1 = 360 | 9-7-56 | (MED)
25
397 |
85 | V | NAVY | MISSILE
(LONG RANGE
TYPHON
MISSILE) | SURFACE-TO-AIR MISSILE . COMPLETELY NEW VERSION OF TALOS AIRFRAME. MODULAR ELECTRONIC PACKAGING.
NOT YET DETERMINED.
(PROBLEM STATEMENT MCDONNELL-1-V, MCDONNELL-1-W, MCDONNELL-1-X, MCDONNELL-1-Y (MCDONNELL REPORT 7513) | 9-7-56 | (MED)
25
303 |
85 | W | NAVY | MISSILE | SURFACE-TO-AIR MISSILE . SAME AS MODELS 85 AND 85A EXCEPT WITH NEW FORWARD BODY CONTAINING FUNDAMENTALLY DIFFERENT ELECTRONIC AND WARHEAD INSTALLATION. REVISED BOOSTER, C-BAND INTELLIGENCE,
(NOW X SAM-N-6AW)
MODEL T [RAMJET] M1 = 2 .2
SC A1 = 225 | 1-29-52 | (MED)
01-26
325 |
85 | X | NAVY | TEST MISSILE | LAUNCHER TEST VEHICLE, VERSION OF MODEL 85W, SAME AS MODEL 85W EXCEPT WITH 233-A2 BOOSTER AND 76.6 INCH BOOSTER FINS. INTELLIGENCE OMITTED.
NONE
(PROBLEM STATEMENT MCDONNELL-1-C) | 2-17-56 | (MED)
325 |
85 | Y
(BPD
4401
4402) | NAVY | MISSILE
(TALOS 6BW1 -
UNITIZED) | SURFACE-TO-AIR MISSILE. PROTOTYPE VERSION OF MODEL 85T. UNITIZED AFT SECTION. STEEL HYDROSPUN DIFFUSER. MODULAR ELECTRONIC PACKAGING . BEAM RIDING GUIDANCE ONLY - NO HOMING.
MODEL J-2L [RAMJET] | 12-17-56 | (MED)
325 |
85 | Z
(BPD
4867) | NAVY | MISSILE
(TALOS 6B1
UNITIZED) | SURFACE-TO-AIR MISSILE. SIMILAR TO MODEL 85N, IN-LINE CONFIGURATION. MODULAR ELECTRONIC PACKAGING, MOUNTING PROVISIONS AFT OF B .S. 105 FOR UNITIZED PACKAGING. HOGGED-OUT PARTS UTILIZED IN FORWARD SECTION. STOWAGE STRONG POINT AT B.S. 105. PROVISION FOR WING CONTROL DURING BOOST. MOUNTING PROVISION FOR STAPFUS. C-BAND INTELLIGENCE (NOW X SAM -N-6B1)
MODEL J - 2L [RAMJET] M1 = 2 .73
SC A1 = 360 | 3-5-57 | (MED)
397 |
85 | AA | NAVY | MISSILE
(TALOS 6C1) | SURFACE-TO-AIR MISSILE. SINGLE STAGE, LONG RANGE, C.W.I. GUIDANCE, WEIGHT REDUCTION ACCOMPLISHED BY USE OF MAGNESIUM AND A REDUCTION IN GAUGE THICKNESS.
MODEL J-2LB RAMJET (LIQUID PROPELLANT) | 7-21-58 | (MED) 397
612
613
805 |