Magnavox MX7221 GPS Receiver

© Brooke Clarke 2013 - 2025

Background
DC Power
Power Up Sequence
Antenna
Photos
Patents
Related
Links

Background

The first GPS satellite was launched in 1978 and the system was fully operational in 1993.  This was a time period when there was a lot of GPS developments. Land surveyors developed methods of using the L2 carrier frequency even though they did not know the secret code to unlock the data.

This is a GPS receiver made in the late 1990s by Magnavox.  It came with an antenna made by Sensor Systems (p/n 627168-1 model S67-1575-29).  It's an L1 civilian frequency only antenna.  1990 & 1991 date codes.

In 2025 discovered the MX 4400 series of GPS receivers.  The brochure is dated 1987 so this model precedes the MX7221 by a few years. 
Adding Patents paragraph.

DC Power

Cable Connector: MS3476W12-10S

Pin
Function
A
+6 - +15 VDC
C
Ground chassis
D
Data
E
Data
B, F, G, H, J, K
nc

Power Up Sequence

The screens are in order top to bottom:


-

25 JUL99 00:00:00
0SAT  STS  TFOM 9
  SELF-TEST  IN
    PROGRESS
O3APR05 00:00:18
0SAT STS  TFOM 9

Antenna

Sensor Systems p/n: 627168-1
                model: S67-1575-29
Sensor Systems p/n: 627168-1
                model: S67-1575-29


Sensor Systems p/n: 627168-1 model:  S67-1575-29 is not on their web page.
Looks like an L1 (1575) only antenna.
Dated: Mar 26 1991
TNC jack.

Photos

Magnavox MX7221 GPS Receiver
RF & Front Panel
Magnavox MX7221
                  GPS Receiver
Note: Dead yellow LTC-7PN Lithium battery
CPU 80C186
U10 & U12 ROMs marked V6.17
implying developed firmware
Magnavox MX7221
                  GPS Receiver
Power Supply & 1 PPS Output
Magnavox MX7221
                  GPS Receiver


Patents

Magnavox - Richard G. Keegan went to work for John Deere after leaving Magnavox and has many patents relating to GPS on tractors.

5040240 Receiver architecture for use with a global positioning system, Richard G. Keegan, Magnavox Government and Industrial Electronics, 1991-08-13, -
Defines F=5.115 MHz (half the now popular frequency of 10.23 MHz).
The received L1 signal is 308 *(F + d) where d is the Doppler offset of the satellite being received.  Received L2 = 240 *(F + d).
All the LOs in the receiver and the sampling clock are derived from a single oscillator thus making for phase coherent signals.

Related

DAGR
PLGR
Navigation


Links

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page page created 19 March 2013.