Validation of a two-way satellite communication system without utilizing a satellite

1. A method of validating a two-way satellite communication system in an aircraft, the method comprising:

providing the two-way satellite communication system in the aircraft, the two-way satellite communication system comprising:

a network access unit to provide network access for a plurality of data devices;

a modem to modulate uplink data received from the network access unit to obtain an uplink signal, and demodulate a downlink signal to obtain demodulated downlink data provided to the network access unit; and

a satellite antenna assembly to transmit the uplink signal, and to receive the downlink signal;

arranging a satellite link emulator proximate the aircraft;

performing a validation test of the two-way satellite communication system using the satellite link emulator, including receiving, at the satellite link emulator, the transmitted uplink signal from the satellite antenna assembly, and transmitting, using the satellite link emulator, the downlink signal to the satellite antenna assembly in response to the received uplink signal; and

determining a pass/fail indication based on operation of the network access unit, the modem, and the satellite antenna assembly during the validation test.

2. The method of claim 1 , wherein determining the pass/fail indication is based on one or more measured signal quality metrics of data traffic communicated in the two-way satellite communication system during the validation test.

3. The method of claim 1 , wherein arranging the satellite link emulator comprises arranging the satellite link emulator on an exterior of the aircraft.

4. The method of claim 1 , wherein performing the validation test of the two-way satellite communication system further includes generating data in the network access unit to simulate data traffic in the two-way satellite communication system.

5. The method of claim 1 , wherein performing the validation test of the two-way satellite communication system further includes receiving data in the network access unit to simulate data traffic in the two-way satellite communication system.

6. The method of claim 5 , wherein performing the validation test of the two-way satellite communication system further includes initiating the validation test using a validation controller, and the received data in the network access unit is from the validation controller.

7. The method of claim 5 , wherein the received data is wirelessly received data in the network access unit.

8. The method of claim 1 , wherein performing the validation test of the two-way satellite communication system further includes performing first communications between the network access unit and the modem and performing second communications between the modem, the satellite antenna, and the satellite link emulator, separate from and independent of the first communications.

9. The method of claim 8 , wherein the pass/fail indication is based on results of each of the first communications and the second communications.

10. The method of claim 1 , wherein performing the validation test of the two-way satellite communication system comprises conducting an electromagnetic interference (EMI) test.

11. An apparatus comprising:

a two-way satellite communication system in an aircraft, the two-way satellite communication system comprising:

a network access unit to provide network access for a plurality of data devices;

a modem to modulate uplink data received from the network access unit to obtain an uplink signal, and demodulate a downlink signal to obtain demodulated downlink data provided to the network access unit;

a satellite antenna assembly to transmit the uplink signal, and to receive the downlink signal; and

a validation system to validate the two-way satellite communication system, the validation system comprising:

a satellite link emulator; and

a validation controller to initiate a validation test of the two-way satellite communication system using the satellite link emulator, the validation test including communicating data traffic in the two-way satellite communication system to cause the satellite antenna assembly to transmit the uplink signal to the satellite link emulator and in response cause the satellite link emulator to transmit the downlink signal to the satellite antenna assembly,

the validation controller further to determine a pass/fail indication based on operation of the network access unit, the modem, and the satellite antenna assembly during the validation test.

12. The apparatus of claim 11 , wherein the pass/fail indication is based on one or more measured signal quality metrics of data traffic communicated in the two-way satellite communication system during the validation test.

13. The apparatus of claim 11 , wherein the satellite link emulator is disposed on an exterior of the aircraft.

14. The apparatus of claim 11 , wherein the validation test further includes the reception of data in the network access unit to simulate the data traffic in the two-way satellite communication system.

15. The apparatus of claim 14 , wherein the received data in the network access unit is from the validation controller.

16. The apparatus of claim 14 , wherein the received data is wirelessly received in the network access unit.

17. The apparatus of claim 11 , wherein the validation test further includes first communications between the network access unit and the modem and second communications between the modem, the satellite antenna, and the satellite link emulator, independent of and separate from the first communications.

18. The apparatus of claim 17 , wherein the pass/fail indication is based on results of each of the first communications and the second communications.

19. The apparatus of claim 11 , wherein the validation system further comprising an electromagnetic interference (EMI) test receiver, and the validation test includes an EMI test.