Human Spaceflight
APOLLO 5 LM APS
DecayedHuman SpaceflightLEO
The ascent propulsion system (APS) or lunar module ascent engine (LMAE) is a fixed-thrust hypergolic rocket engine developed by Bell Aerosystems for use in the Apollo Lunar Module ascent stage. It used Aerozine 50 fuel, and N2O4 oxidizer. Rocketdyne provided the injector system, at the request of NASA, when Bell could not solve combustion instability problems.
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Launch
- Launch date
- January 22, 1968 at 10:48 PM UTC
- Launch site
- Cape Canaveral SFS, USA
- Launched by
- Saturn IB →
- Operator
- National Aeronautics and Space Administration
- Mission
- Apollo 5
- Launch record
- View full launch →
Orbit
- Orbit regime
- LEO
- Apoapsis
- 222 km
- Periapsis
- 158 km
- Inclination
- 31.61°
- Orbital period
- 88.3 min
Spacecraft
- Operator
- United States
- Launch mass
- 4,705 kg
Identity
- COSPAR (Int'l)
- 1968-007A
- NORAD catalog №
- 3106
- Object type
- Payload
- Owner / operator
United States- Status
- Decayed
- Decay / reentry
- January 24, 1968
End of mission
- Last active / ended
- January 24, 1968
- Time in service
- 2 days
- Fate
- Reentered Earth's atmosphere and was destroyed.
- Final status
- Decayed