AS-202

AS-202 was the third test flight of the Saturn IB, because a delay in the readiness of the Apollo spacecraft 011 pushed its launch past the July 1966 launch of AS-203. It was designed to test the rocket more than had been done on AS-201 by launching the rocket higher and having the flight lasting twice as long. It would also test the command and service module (CSM-011) by having the engine fire four times during the flight. The flight was also designed to test the heat shield by subjecting it to 260 megajoules per square meter. Over the course of the reentry it generated equivalent energy needed to power Los Angeles for over one minute in 1966. CSM-011 was basically a production model capable of carrying a crew. However it lacked the crew couches and some displays that would be included on later missions for the astronauts. This was the first flight of the guidance and navigation system as well as the fuel cell electrical system. ==Flight==

AS-202 was launched 25 August 1966 from Pad 34. The launch phase was perfectly nominal with the first stage burning for just under two and a half minutes, lifting the rocket to an altitude of , downrange from the launch pad. The second stage then burned for a further seven and a half minutes, putting the spacecraft into a ballistic trajectory. The CSM was separated from the rocket stage at an altitude of . The CSM was preprogrammed to make four burns of its service propulsion system (SPS). The first occurred a couple of seconds after separation from the S-IVB second stage. It burned for 3 minutes, 35 seconds, lifting the spacecraft apogee to , downrange. The second burn was 25 minutes later, lasting one minute 28 seconds. Ten seconds later, two more burns of three seconds each were done to test the rapid restart capabilities of the engine. The command module entered the atmosphere at a speed of . The spacecraft performed a skip reentry, first descending to , then lifting back up to . By this time it had shed of speed. It then continued to descend. The main parachutes deployed at . It splashed down at , from the target landing site, and the aircraft carrier took 8 hours and 30 minutes to reach the capsule (approximately southeast of Wake Island). ==Staging footage==

AS-202 was one of three uncrewed Apollo missions which obtained notable close-up footage of a Saturn rocket during staging, the others being Apollo 4 and Apollo 6. Ejectable cameras were mounted to each launch vehicle, technology first developed for the Saturn I. On AS-202, a camera was mounted to the Saturn IB vehicle's first stage, the S-IB, looking forward. It captured footage of the vehicle's second stage, the S-IVB (200 series) pulling away and firing its single J-2 engine. The upper stage is identifiable by its firing of three ullage motors; a later iteration of the S-IVB, the 500 series, had only two ullage motors, and was that used on Saturn V launches. Although the footage was captured during an uncrewed flight, it is frequently used as stock footage in documentaries of crewed flights, to illustrate staging. The footage was used in the documentary film Apollo 11, and is sometimes erroneously attributed to Apollo 11, or other crewed missions. ==Museum display==

The capsule was displayed in the US Pavilion at Expo 67 in Montreal. The capsule is currently on display aboard . The ship is open to the public as the USS Hornet Museum in Alameda, California. File:USS Hornet Apollo CM.jpg|AS-202 CM-011 exhibited on USS Hornet File:Apollo Capsule (USS Hornet).jpg|AS-202 CM-011 interior ==References==