Apollo 5
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From Simple English Wikipedia, the free encyclopedia
Lunar Module 1 being mated to the Spacecraft Lunar Module Adapter (SLA) in preparation for launch as Apollo 5 | |
| Mission type | Lunar module test flight |
|---|---|
| Operator | NASA |
| COSPAR ID | Ascent stage: 1968-007A Descent stage: 1968-007B |
| SATCAT no. | 3106 |
| Mission duration | 11 hours, 10 minutes |
| Orbits completed | 7 |
| Spacecraft properties | |
| Spacecraft | Apollo LM-1 |
| Manufacturer | Grumman |
| Launch mass | 14,360 kilograms (31,660 lb)[1] |
| Start of mission | |
| Launch date | January 22, 1968, 22:48:09 (1968-01-22UTC22:48:09Z) UTC |
| Rocket | Saturn IB SA-204 |
| Launch site | Cape Kennedy LC-37B |
| End of mission | |
| Disposal | Uncontrolled reentry |
| Deactivated | January 23, 1968 9:58 (1968-01-23UTC09:59Z) UTC |
| Decay date | Ascent stage: January 24, 1968 (1968-01-25) Descent stage: February 12, 1968 (1968-02-13) |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth orbit |
| Perigee | 162 kilometers (87 nmi)[2] |
| Apogee | 214 kilometers (116 nmi)[2] |
| Inclination | 31.6 degrees[2] |
| Period | 89.5 minutes[2] |
| Epoch | January 22, 1968 (ascent stage)[3] |
Apollo 5 was the first unmanned test flight of the Apollo Lunar Module.[4] The Apollo Lunar Module was the lander part of Apollo spacecraft. The module was launched in
January 22, 1968 from Cape Canaveral Air Force Station.[4]
References
[change | change source]- | "Apollo 5". NASA Space Science Data Coordinated Archive. Archived from the original on January 8, 2017. Retrieved September 26, 2016.
- 1 2 3 4 "Apollo 5". NASA Space Science Data Coordinated Archive. Archived from the original on October 1, 2016. Retrieved September 26, 2016.
- | McDowell, Jonathan. "SATCAT". Jonathan's Space Pages. Retrieved March 23, 2014.
- 1 2 "Apollo 5". NASA NSSDC. Archived from the original on 2017-01-08. Retrieved 2012-01-16.
