AKA: Lunar module Test Article. Status: Operational 1967.
Several were used in test flights of Saturn launch vehicles, most famously in Apollo 8.
On August 12 Kraft informed Low that December 20 was the day if they wanted to launch in daylight. With everyone agreeing to a daylight launch, the launch was planned for December 1 with a "built-in hold" until the 20th, which would have the effect of giving assurance of meeting the schedule. LTA (LM test article)-B was considered as a substitute; it had been through a dynamic test vehicle program, and all except Kotanchik agreed this would be a good substitute. Grumman suggested LTA-4 but Low decided on LTA-B.
George M. Low, ASPO Manager, set forth the rationale for using LTA-B (as opposed to some other LM test article or even a full-blown LM) as payload ballast on the AS-503 mission. That decision had been a joint one by Headquarters, MSFC, and MSC. Perhaps the chief reason for the decision was Marshall's position that the Saturn V's control system was extremely sensitive to payload weight. Numerous tests had been made for payloads of around 38,555 kilograms but none for those in the 29,435- to 31,750-kilogram range. MSFC had therefore asked that the minimum payload for AS-503 be set at 38,555 kilograms. Additional Details: here....
Apollo 7 - flown October 11-22 - far exceeded Low's expectations in results and left no doubts that they should go for lunar orbit on Apollo 8. At the November 10 Apollo Executive meeting Phillips presented a summary of the activities; James gave the launch vehicle status; Low reported on the spacecraft status and said he was impressed with the way KSC had handled its tight checkout schedule; Slayton reported on the flight plan; and Petrone on checkout readiness. Petrone said KSC could launch as early as December 10 or 12. Phillips said he would recommend to the Management Council the next day for Apollo 8 to go lunar orbit. Additional Details: here....