|
AAP |
Apollo Applications Program |
|
AM |
Airlock Module |
|
ATM |
Apollo Telescope Mount |
|
CECO |
Center Engine Cutoff |
|
CSM |
Command and Service Module |
|
CW |
Clockwise |
|
EBW |
Exploding Bridge Wire |
|
ECP |
Engineering Change Proposal |
|
EMR |
Engine Mixture Ratio |
|
g |
Gravity |
|
IU |
Instrument Unit |
|
IGM |
Iterative Guidance Mode |
|
JSC |
Johnson Space Center |
|
KSC |
Kennedy Space Center |
|
LSC |
Linear Shaped Charged |
|
MAX-Q |
Maximum Dynamic Pressure |
|
MDA |
Multiple Docking Adapter |
|
MDAC |
McDonnell Douglas Astronautics Company |
|
MDAC-W |
McDonnell Douglas Astronautics Company-West |
|
MS |
Meteoroid Shield |
|
ms |
millisecond |
|
MSFC |
Marshall Space Flight Center |
|
OECO |
Outboard Engine Cutoff |
|
OWS |
Orbital Workshop |
|
R |
Range Time |
|
S-IB |
Saturn IB, First Stage |
|
S-IC |
Saturn V, First Stage |
|
S-II |
Saturn V, Second Stage |
|
S-IVB |
Saturn IB, Second Stage |
|
S-V |
Saturn V |
|
SA-513 |
Launch Vehicle for Skylab 1 |
|
SAS |
Solar Array System |
|
SAS-1 |
Solar Array System 1 |
|
SAS-2 |
Solar Array System 2 |
|
SL-1 |
Skylab 1 |
|
SL-2 |
Skylab 2 |
|
STA |
Static Test Article |
|
SWS |
Saturn Workshop |
|
TACS |
Thruster Attitude Control Subsystem |
|
Vdc |
Volts Direct Current |
|
w |
watts |