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AS-203 (also known as SA-203 or Apollo 3) was an uncrewed flight of the Saturn IB rocket on July 5, 1966. It carried no command and service module, as its purpose was to verify the design of the S-IVB rocket stage restart capability that would later be used in the Apollo program to boost astronauts from Earth orbit to a trajectory towards the Moon. It…
Art, Objectives & Flight
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s-ivb launch design saturn orbit stage apollo rocket would flight objectives orbits cape kennedy tank two test vehicle spacecraft ib
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| AS-203 | Apogee altitude | 214 kilometers (116 nmi) | 1.00 | infobox |
| AS-203 | COSPAR ID | 1966-059A | 1.00 | infobox |
| AS-203 | Destroyed | July 5, 1966 (1966-07-06) | 1.00 | infobox |
| AS-203 | Distance travelled | 161,900 kilometers (87,400 nmi) | 1.00 | infobox |
| AS-203 | Epoch | July 5, 1966 | 1.00 | infobox |
| AS-203 | Inclination | 31.94 degrees | 1.00 | infobox |
| AS-203 | Launch date | July 5, 1966, 14:53:13 (1966-07-05UTC14:53:13Z) UTC | 1.00 | infobox |
| AS-203 | Launch site | Cape Kennedy LC-37B | 1.00 | infobox |
| AS-203 | Mission duration | ~6 hours | 1.00 | infobox |
| AS-203 | Mission type | Launch vehicle development | 1.00 | infobox |
| AS-203 | Operator | NASA | 1.00 | infobox |
| AS-203 | Orbits completed | 4 | 1.00 | infobox |
| AS-203 | Perigee altitude | 184 kilometers (99 nmi) | 1.00 | infobox |
| AS-203 | Period | 88.47 minutes | 1.00 | infobox |
| AS-203 | Reference system | Geocentric | 1.00 | infobox |
| AS-203 | Regime | Low Earth orbit | 1.00 | infobox |
| AS-203 | Rocket | Saturn IB SA-203 | 1.00 | infobox |
| AS-203 | SATCAT no. | 2289 | 1.00 | infobox |
| AS-203 | Spacecraft | None | 1.00 | infobox |
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