Scenario File Options

The Project Apollo scenarios have a vast number of options that you can specify. Some of the more useful are:

General options

These are options specifying things such as the fuel mass, the intended orbit after launch, etc.

Option	Function
TOAPO	Specifies the desired launch apogee altitude in kilometers.
TOPER	Specifies the desired launch perigee altitude in kilometers.
TOHDG	Specifies the desired launch azimuth in degrees.
TCP	Specifies the height of the rocket above the ground in meters prior to launch. This can be adjusted if the mission is flown from a different launch pad to the default for the spacecraft (e.g. the Skylab 'milk stool' for the Saturn 1b).
APOLLONO	Apollo mission number. This is used to provide mission-specific events such as mission audio or system failures.
VECHNO	The Saturn vehicle number: typically this will be in the 200s for a Saturn 1b, and 500s for a Saturn V. This is used to name the separated stages and components of the spacecraft.
REALISM	Sets the realism level from 0 (lowest) to 10 (highest). Lower realism level missions will be easier to fly. Quickstart mode is level 0, Standard mode is level 5.
DLS	Set to 1 to delete the launch site when the spacecraft passes out of visible range. This can give a significant performance boost on slow machines.
FDAIDISABLED	Set to 1 to disable the OpenGL FDAI rendering. This can give a significant performance boost on slow machines.
HASPROBE	Allows you to override the default docking probe state. Set to 1 if the spacecraft has a docking probe, or 0 if it doesn't.
MISSNTIME	Current mission time in seconds since launch.
IGMST	Inertial Guidance Mode start: set to the time in seconds after launch at which the autopilot switches to inertial guidance mode and starts trying to hit the target orbit rather than follow the pre-planned pitch program.
SIFUELMASS	Specifies the mass in kilograms of the fuel in the first stage (S-IC or S-IB).
SIEMPTYMASS	Specifies the empty mass in kilograms of the first stage (S-IC or S-IB).
SICSHUT	Specifies the mission time of center engine shutdown of the first stage (S-IC or S-IB).
SISHUT	Specifies the mission time of shutdown of the remaining engines of the first stage (S-IC or S-IB).
SIIFUELMASS	Specifies the mass in kilograms of the fuel in the second stage (S-IVB for Saturn 1B or S-II for Saturn V). This is not used for the INT-20.
SIIEMPTYMASS	Specifies the empty mass in kilograms of the second stage (S-IVB for Saturn 1B or S-II for Saturn V). This is not used for the INT-20.
SIICSHUT	Specifies the mission time of the center engine shutdown of the S-II stage of Saturn V and derivatives.
SIIPUT	Specifies the mission time of the PU-shift (change of mixture ratio) the second stage (S-IVB for Saturn 1B or S-II for Saturn V).
SIISHUT	Specifies the mission time of shutdown of the remaining engines of the S-II stage of Saturn V and derivatives.
S4FUELMASS	Specifies the mass in kilograms of the fuel in the S-IVB stage of Saturn V and derivatives.
SMMASS	Empty mass of the Service Module, in kilograms.
CMMASS	Empty mass of the Command Module, in kilograms.
S4PL	Specifies the payload of the SIVb stage. Current values are: 0 Standard LEM 1 ASTP 2 LTA LEM test article 3 LM1 test LEM 4 LTA8 LEM test article 5 Docking target 6 LTA6 LEM test article 7 Empty 8 Docking adapter for an SIVb 'wet workshop'
AUTOSLOW	Set to 1 to slow to 1x time acceleration when 'something important' happens. For manned flights, this is typically when a piece of mission audio is played, for unmanned flights it is typically a stage separation, engine burn, etc.
MOONLAT	Latitude (in degrees) of the planned landing site on the Moon, if any.
MOONLONG	Longitude (in degrees) of the planned landing site on the Moon, if any.
MOONALT	Altitude (in meters) of the planned landing site on the Moon, if any.
LANDFAIL	Landing failures. Set to 1 to disable all random landing failures in your scenario, or 0 to create a random set of failures.
LAUNCHFAIL	Launch failures. Set to 1 to disable all random launch failures in your scenario, or 0 to create a random set of failures.
SWITCHFAIL	Switch failures. Set to 1 to disable all random switch failures in your scenario, or 0 to create a random set of failures.
UNMANNED	Set to 1 for an unmanned mission.
LEMN	Set to the LEM vessel name (e.g. Eagle for Apollo 11). This is the name the LEM will be given when it is created.

Audio options

Option	Function
LANG	Set to the appropriate string for the audio language you want to use. Currently we only ship English audio, but if, say, you downloaded a French audio add-on you could set this to French instead and the French files would take precedence.

AGC options

AGC options are specified between AGC_BEGIN and AGC_END. Options outside those lines will be ignored.

Option	Function
YAAGC	Set to 1 to use the Virtual AGC rather than the C++ AGC
EMEM	Set an AGC erasable memory location to a specified value. Addresses and values are both specified in octal (base-8), so to set address 10 (decimal) to 17 (decimal) you would specify EMEM0012 21. In general you should use LMPAD and CMPAD instead of specifying specific memory locations as both C++ AGC and Virtual AGC use the same scenario values to store different data.

Virtual AGC options

These options are set in the standard CSM configuration, not between the AGC_BEGIN and AGC_END lines. If you try to set them inside the AGC configuration they will be ignored.

Option	Function
CMPAD	Set a Virtual AGC erasable memory location in the CM AGC to a specified value. Addresses and values are both specified in octal (base-8), so to set address 10 (decimal) to 17 (decimal) you would specify EMEM0012 21. If the scenario uses the C++ AGC rather than Virtual AGC, these values are ignored. CMPAD entries are used once to set up the values in the AGC when the scenario is loaded, then thrown away. So they will not be saved to a scenario file when you exit Orbiter.
LMPAD	Set a Virtual AGC erasable memory location in the LM AGC to a specified value. Addresses and values are both specified in octal (base-8), so to set address 10 (decimal) to 17 (decimal) you would specify EMEM0012 21. If the scenario uses the C++ AGC rather than Virtual AGC, these values are ignored. Note that the LEM PAD is loaded when the LEM is created, so setting these values when the LEM already exists in the scenario will have no effect.
LMPADCNT	Sets the number of LEM PAD entries. The LEM PAD is saved in a table until the LEM is created, so the DLL needs to know how large a table to create. Any values beyond this count will be ignored.

Scenario information

These values aren't typically set in a newly created scenario, but are saved to the scenario from the DLL when exiting Orbiter.

Option	Function
NASSPVER	This gives the version number of the DLL which saved the scenario... for 7.0 it's 70000.

See Also

• Config File Options