• The first Soviet flight to he moon will use the current plan - one N1 launch, one cosmonaut on the moon.
• Special measures must be taken to ensure the safety of that single cosmonaut
• A new N1 model is to be developed to land the new L5 spacecraft (which will be able to handle 4 to 5 crew, 1.5 to 2.0 tonnes of scientific equipment, and spend three months on the lunar surface). This is to be ready two to three years after the first landing.
• The Academy of Sciences, the Ministry of Defence, and MOM are to develop a program of military and scientific experiments to be carried aboard the L3
• The next meeting of the lunar soviet will be in November/December 1967

Main objectives of the mission were to demonstrate the structural and thermal integrity of the space vehicle and to verify adequacy of the Block II heatshield design for entry at lunar return conditions. These objectives were accomplished.

The S-IC stage cutoff occurred 2 minutes 30 seconds into the flight at an altitude of about 63 kilometers. The S-II stage ignition occurred at 2 minutes 32 seconds and the burn lasted 6 minutes 7 seconds, followed by the S-IVB stage ignition and burn of 2 minutes 25 seconds. This series of launch vehicle operations placed the S-IVB and spacecraft combination in an earth parking orbit with an apogee of about 187 kilometers and a perigee of 182 kilometers. After two orbits, which required about three hours, the S-IVB stage was reignited to place the spacecraft in a simulated lunar trajectory. This burn lasted five minutes. Some 10 minutes after completion of the S-IVB burn, the spacecraft and S-IVB stage were separated, and less than 2 minutes later the service propulsion subsystem was fired to raise the apogee. The spacecraft was placed in an attitude with the thickest side of the CM heatshield away from the solar vector. During this four-and-one-half-hour cold-soak period, the spacecraft coasted to its highest apogee - 18,256.3 kilometers. A 70 mm still camera photographed the earth's surface every 10.6 seconds, taking 715 good-quality, high-resolution pictures.

About 8 hours 11 minutes after liftoff the service propulsion system was again ignited to increase the spacecraft inertial velocity and to simulate entry from a translunar mission. This burn lasted four and one half minutes. The planned entry velocity was 10.61 kilometers per second, while the actual velocity achieved was 10.70.

Recovery time of 2 hours 28 minutes was longer than anticipated, with the cause listed as sea conditions - 2.4-meter swells. References: 2, 6, 16, 26, 27.

• Development of crew safety items, cockpit indicators on the function of the landing system, and controls for manual landing by the astronaut
• Development of the HAZ complex for training of crew members
• Review and approval of station systems for water generation, medical observation of the crew, and atmosphere indicators and controls
• Development of a manned manoeuvring unit to allow the cosmonauts to manoeuvre up to 300 m from the station

• CSM 020 would be flown on the Apollo 6 mission.
• Boilerplate 30 was assigned to the AS-503 unmanned mission.
• If Apollo 6 was successful, AS-503 would be flown as the first Saturn V manned mission.