D-17B

High reliability was required of the D-17B. It controlled a key weapon that would have just one chance to execute its mission. Reliability of the D-17B was achieved through the use of solid-state electronics and a relatively simple design. Simpler DRL (diode–resistor) logic was used extensively, but less-reliable DTL (diode–transistor) logic (which provides gain and inversion) was used only where needed. In the late 1950s and early 1960s, when the D-17B was designed,[1] transistors lacked today's reliability. Reliability was also enhanced by the rotating-disk memory with non-destructive readout (NDRO). In actual real-time situations, Minuteman missiles achieved a mean time between failures (MTBF) of over 5.5 years .

The Soviets had much larger rockets and could use vacuum tubes in their guidance systems. (The weights of the Minuteman I and II remain classified, but the Minuteman III was 35,000 kg versus the Soviet R-7 missile (1959) of 280,000 kg.) The US planners had to choose either to develop solid state guidance systems (which weigh less) or consider the additional cost and time delay of developing larger rockets.

Minuteman I D-17B computer specifications

Year: 1962

The D17B is a synchronous serial general-purpose digital computer.

Manufacturer: Autonetics Division of North American Aviation

Applications: Guidance and control of the Minuteman I ICBM.

Programming and numerical system:

Number system: Binary, fixed point, 2's complement

Logic levels: 0 V for logical 0 (false), -10 V for logical 1 (true)

Data word length (bits): 11 or 24 (double precision)

Instruction word length (bits): 24

Binary digits/word: 27

Instructions/word: 1

Instruction type: One and half address

Number of instructions: 39 types from a 4-bit op code by using five bits of the operand address field for instructions which do not access memory.

Execution times in microseconds:

Add: 78+1⁄8 µs

Multiply: 546+7⁄8 µs or 1,015+5⁄8 µs (double precision)

Divide: (software)

(Note: Parallel processing such as two simultaneous single precision operations is permitted without additional execution time.)

Clock channel: 345.6 Hz

Addressing:

Direct addressing of entire memory

Two-address (unflagged) and three-address (flagged) instructions

Memory:

Word length (bits): 24 plus 5 timing

Type: Ferrous-oxide-coated NDRO disk

Cycle time: 78+1⁄8 µs (minimal)

Capacity (words): 5,454 or 2,727 (double precision)

Input/output:

Input lines: 48 digital

Output lines: 28 digital

12 analog

3 pulse

Program: 800 5-bit char/s

Instruction word format:

    +--------+--------+------+--------+---------+--------+--------+
    |   TP   | T24 21 | 20   | 19  13 | 12    8 | 7    1 |   0    |
    +--------+--------+------+--------+---------+--------+--------+
    | Timing | OP     | Flag | Next   | Channel | Sector | Timing |
    |        |        |      | Inst.  |         |        |        |
    |        |        |      | Sector |         |        |        |
    +--------+--------+------+--------+---------+--------+--------+

Registers:

Phase and voltage output registers

Construction (arithmetic unit only): transistor-diode logic is used.

Timing: Synchronous

Operation: Sequential

Input

48 digital lines (input)

26 specialized incremental inputs

   -Medium-             -Speed-
   Paper/Mylar Tape      600 chars/sec
   Keyboard              Manual
   Typewriter            Manual

Output

   -Medium-              -Speed-
   Printer Character     78.5–2,433 ms   (Program Control)
   Phase - Voltage       (Program Control)

28 digital lines (output) 12 analog lines (output) 13 pulse lines (output) 25,600 word/s maximum I/O transfer rate

Physical characteristics

Dimensions: 20 in high, 29 in diameter, 5 in deep

Power: 28 VDC at 25 A

Circuits: DRL and DTL

Weight: 62 pounds (28 kg)

Construction:

Double copper clad, gold plated, glass fiber laminate, flexible polyurethane-coated circuit boards

Software:

Minimal delay coding using machine language

Modular special-purpose subroutines

Reliability: 5.5 years MTBF

Checking features: Parity on fill and on character outputs

Power, space, weight, and site preparation

Power, computer: 0.25 kW

Air conditioner: Closed system

Volume, computer: 1.55 cu ft (44 L)

Weight, computer: 70 lb (32 kg)

Designed specifically to fit in cylindrical guidance package.

The word length for this computer Is 27 bits, of which 24 are used In computation. The remaining 3 bits are spare and synchronizing bits. The memory storage capability consists of a 6000 rpm magnetic disk with a storage capacity of 2985 words of which 2728 are addressable. The contents of memory include 20 cold-storage channels of 128 sectors (words) each, a hot-storage channel of 128 sectors, four rapid access loops (U,F,E,H) of 1, 4, 8, and 16 words respectively, four 1-word arithmetic loops (A, L,H,I), and a two 4-word input buffer input loops (V,R).

The outputs that can be realized from the D-17B computer are binary, discrete, single character, phase register status, telemetry, and voltage outputs. Binary outputs are computer generated levels of +1 or −1 available on the binary output lines.

D-17B Instruction Repertoire

Numeric Code		Code	Description
------------		----	-----------
00 20, s 		SAL 	Split accumulator left shift
00 22, s 		ALS 	Accumulator left shift
00 24, 2 		SLL 	Split left word left shift
00 26, r 		SLR 	Split left word right shift
00 30, s 		SAR 	Split accumulator right shift
00 32, s 		ARS 	Accumulator right shift
00 34, s 		SRL 	Split right word left shift
00 36, s 		SRR 	Split right word right shift
00 60, s 		COA 	Character output A
04  c, S 		SCL 	Split Compare and .ivt
10  c, S 		TMI 	Transfer on minus
20  c, s 		SMP 	Split multiply
24  c, s 		MPY 	Multiply
30  c, s 		SMM 	Split multiply modified
34  c, s 		MPM 	Multiply modified
40 02, s 		BOC 	Binary output C
40 10, s 		BCA 	Binary output A
40 12, s 		BOB 	Binary output B
40 20, s 		RSD 	Reset detector
40 22, s 		HPR 	Halt and Proceed
40 26, s 		DOA 	Discrete output A
40 30, s 		VOA 	Voltage output A
40 32, s 		VOB 	Voltage output B
40 34, s 		VOC 	Voltage output C
40 40, s 		ANA 	And to accumulator
40 44, s 		MIM 	Minus magnitude
40 46, s 		COM 	Complement
40 50, s 		DIB 	Discrete input B
40 52, s 		DIA 	Discrete input A
40 60, s 		HFC 	Halt fine countdown
40 62, s 		EFC 	Enter fine countdown
40 70, s 		LPR 	Load phase register
44  c, s 		CIA 	Clear and Add
50  c, s 		TRA 	Transfer
54  c, s 		STO 	Store accumulator
60  c, s 		SAD 	Split add
64  c, s 		ADD 	Add
70  c, s 		SSU 	Split subtract
74  c, s 		SUB 	Subtract

D-17B computer architecture block diagram.

Special features of the D-17B computer include flag store, split-word arithmetic, and minimized access timing. Flag store provides the capability of storing the present contents of the accumulator while executing the next Instruction. Split-word arithmetic is used in performing arithmetic operations on both halves of a split word at the same time. A split word on the D-17B consists of 11 bits. Minimized access timing is the placing of instructions and data in memory so that they are available with minimum delay from the disk memory.

Autonetics was the associate contractor for the Minuteman (MM) guidance system, which included the flight and prelaunch software. This software was programmed in assembly language into a D17 disk computer. TRW provided the guidance equations that Autonetics programmed and was also responsible for the verification of the flight software. When MM I became operational, the flight computer was the only digital computer in the system. The targeting was done at Strategic Air Command (SAC) Headquarters by the Operational Targeting Program developed by TRW to execute on an IBM 709 mainframe computer.[2]

Sylvania Electronics Systems was selected to develop the first ground-based command and control system using a programmable computer. They developed the software, the message processing and control unit for Wing 6. To support the deployment of the Wing 6 system, TRW, Inc. developed the execution plan program (EPP) from a mainframe computer at SAC and performed an independent checkout of the command and control software. The EPP assisted in assigning targets and launch time for the missiles.[2]

The MM II missile was deployed with a D-37C disk computer. Autonetics also programmed functional simulators and the code inserter verifier that was used at Wing headquarters to generate and test the flight program codes to go into the airborne computer.[2]

• Autonetics Division of North American Rockwell. Inc.; Minuteman D-17 Computer Training Data. Anaheim, California, 8 June 1970.
• Autonetics Division of North American Rockwell. Inc.; Part I - Preliminary Maintenance Manual of the Minuteman D-17A Computer and Associated Test Equipment. P.O. Memo 71. Anaheim, California, Inc., January 1960.
• Beck, C.H. Minuteman Computer Users Group, Report MCUG-l-71. New Orleans, Louisiana: Tulane University, April 1971.
• Beck, C.H. Minuteman Computer Users Group. D-17B Computer Programming Manual. Report MCUG-4-71. New Orleans: Tulane University, September 1971.
• Beck, Charles H. Investigation of Minuteman D-17B Computer Reutilization. Available from NTIS/DTIC as document AD0722476, January 1971, 54 pp.
• Lin, Tony C.; "Development of U.S. Air Force Intercontinental Ballistic Missile Weapon Systems." Journal of Spacecraft and Rockets, vol. 40, no. 4, 2003. pp. 491–509.
• Weik, Martin H. (Jan 1964). "MINUTEMAN". ed-thelen.org. A Fourth Survey of Domestic Electronic Digital Computing Systems. Ballistic Research Laboratories, Aberdeen Proving Ground.

• D-37C
• D37D

• "Documents about D-17(B) (mostly) and D-37C". www.bitsavers.org.