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{{Infobox add-on
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'''NASA's Apollo Space Simulation Project''' is an [[Addon]] for Orbiter which recreates the [[Apollo]] missions.
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| 1 = [https://sourceforge.net/projects/nassp/ SourceForge]
 
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| 2 = Team project
 
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| 3 = 7.0 (stable), 8.0 (beta)
 
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| 4 = Orbiter 2010 (7.0), Orbiter Beta (8.0)
 
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}}
 
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'''Project Apollo for Orbiter''' (formerly known as '''NASA's Apollo Space Simulation Project''' or short: '''NASSP''') is an [[add-on]] for [[Orbiter]] which features in-depth and accurate simulation of the [[Apollo]] missions.
 
  
 
==Background==
 
==Background==
  
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NASSP was originally developed by Jean-Luc Rocca-Serra, who released the source code to version 4.x. Mark Grant then rewrote the code as C++, added an initial C++ implementation of the Apollo Guidance Computer, and replaced the control panel bitmaps with new ones from P64. He subsequently released 'NASSP COSTAM' and a derivative which provided basic support for the Virtual AGC software.
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NASSP was originally developed by Jean-Luc Rocca-Serra, who released the source code to version 4.x. Mark Grant then rewrote the code as C++, added an initial C++ implementation of the Apollo Guidance Computer and replaced the control panel bitmaps, releasing 'NASSP COSTAM' and a derivative which provided basic support for the Virtual AGC software.
  
 
Jean-Luc released NASSP 5.0, an updated version based on that source code, for the next release of Orbiter, including, for example, new particle exhaust support and a Skylab launch module.
 
Jean-Luc released NASSP 5.0, an updated version based on that source code, for the next release of Orbiter, including, for example, new particle exhaust support and a Skylab launch module.
  
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With the 6.x release it became ''Project Apollo for Orbiter'', an open source Apollo simulation add-on: for simplicity, both software variants are described here as NASSP. The latest 'stable' version is 7.0.
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With the 6.x release it became ''Project Apollo for Orbiter'', an open source Apollo simulation add-on: for simplicity, both software variants are described here as NASSP. The latest 'stable' version is 6.4.3.
  
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The 8.0 release is currently in beta, including a near-complete simulation of the command module control panel and most of the internal systems, and support for new spacecraft. It is also capable of flying most of an Apollo mission using the Virtual AGC software.
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The 7.0 release is currently in Beta, including a near-complete simulation of the Command Module control panel and most of the internal systems, and support for new spacecraft. It is also capable of flying most of an Apollo mission using the Virtual AGC software.
  
 
==Features==
 
==Features==
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====Early NASSP====
 
====Early NASSP====
  
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Versions prior to 3.0 seem to be unavailable on the web. If anyone has a copy and can update this and/or add screenshots, please do so, or at least let us know what the differences are.
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List To Be Compiled...
  
 
====NASSP 3.x====
 
====NASSP 3.x====
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* Rewritten to use Orbiter docking support.
 
* Rewritten to use Orbiter docking support.
  
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NASSP 3.0 still runs under Orbiter 2006, with no modifications required.
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As a side-note, NASSP 3.0 still runs under Orbiter 2006, with no modifications required.
  
 
====NASSP 4.x====
 
====NASSP 4.x====
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* Engine Gimbal control for all rocket stages, Service module and LEM.
 
* Engine Gimbal control for all rocket stages, Service module and LEM.
 
* Totally rewritten Autopilot (a semi auto mode is available for engine control only).
 
* Totally rewritten Autopilot (a semi auto mode is available for engine control only).
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* New Saturn V and Saturn 1b meshes.
 
 
* Optional high-res Saturn V and Saturn 1b meshes.
 
* Optional high-res Saturn V and Saturn 1b meshes.
 
* Docking system enhancement etc...
 
* Docking system enhancement etc...
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* Revised launch autopilot for increased accuracy.
 
* Revised launch autopilot for increased accuracy.
 
* Same functionality level for Saturn V and Saturn 1b.
 
* Same functionality level for Saturn V and Saturn 1b.
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* NASSP-specific solar system configuration.
 
  
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NASSP 5.x does not currently run under Orbiter 2006 as its Solar System files are incompatible with the new Orbiter format. It could probably be made to run with some changes to the config files.
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NASSP 5.x does not currently run under Orbiter 2006 as it uses its own Solar System which is incompatible with the new Orbiter format. It could probably be made to run with some changes to the config files.
  
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As an extension to NASSP Rodion M. Herrera and others did the NEP (NASSP Enhancement Pack), which contains lunar landing scenarios and mission-specific astronauts etc. A modified NEP version is still available for Project Apollo - NASSP 6.4.3.
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====NASSP 6.x====
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Also, there was an experimental Virtual AGC integration add-on called Virtual Apollo based on Mark Grant's NASSP_COSTAM v2. Meanwhile, it's obsolete and replaced by the Virtual AGC mode in Project Apollo - NASSP. The [http://nassp.sourceforge.net/user/virtualapollo/ documentation] is still online.
 
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=== NCPP 1.0 ===
 
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NCPP (NASSP Complete Panel Project) was done by Matthias and Fabian Müller based on NASSP 5.2 and was the first version with realistic panels. Compared to the panels in the 7.0 beta, which are done by Matthias and Fabian Müller, too, it was only a beginning, of course.
 
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* New CSM and LM control panel
 
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====Project Apollo - NASSP 6.x====
 
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At the beginning of 2005 Jean-Luc Rocca-Serra wasn't able to further develop NASSP and the add-on began to scatter a little bit. Additionally to NASSP 5.2 and NEP 1.0 meanwhile, there was NCPP 1.0 and later on NASSP 6.1, which was an enhancement/fix of NCPP 1.0 for Orbiter 2005. Because all these add-ons depended on each other, at the worst time the user needed to install 7 or 8 files from 3 sites in a certain order. It was so weird that Dan Stephan wrote a quite adequate article about that on his site: "Houston, this add-on has a problem..."
 
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At that point, some people (like Mark Grant, Matthias Müller, etc.) decided to move NASSP to SourceForge as a GNU GPL licensed open source project to save NASSP from vanishing completely and to make team development possible. At that point we wanted to rename the add-on to the more intuitive name "Project Apollo", but this project name wasn't available at SourceForge so we made a compromise and took NASSP as project "unix name" (SourceForge term for the unique project name used for URLs etc.) and "Project Apollo - NASSP" as project title and bundled all these components together for the 6.3 release.
 
  
 
* Rebuilt for 2005 Orbiter release.
 
* Rebuilt for 2005 Orbiter release.
 
* Basic virtual cockpit view.
 
* Basic virtual cockpit view.
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* New control panel.
 
 
* Initial support for unmanned Saturn test flights.
 
* Initial support for unmanned Saturn test flights.
 
* More SIVB payloads.
 
* More SIVB payloads.
 
* Basic LEM ascent autopilot.
 
* Basic LEM ascent autopilot.
 
* Improved AGC emulation.
 
* Improved AGC emulation.
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* Improved Saturn 1B autopilot.
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* Improved Saturn 1b autopilot.
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* More realistic command module aerodynamics.
 
  
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====Project Apollo - NASSP 7.0====
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====NASSP 7 (beta)====
  
 
[[Image:NASSP-panel.jpg|thumb|right|NASSP 7.0 control panel]]
 
[[Image:NASSP-panel.jpg|thumb|right|NASSP 7.0 control panel]]
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* Fully functional 2D Panel Support throughout the CM.
 
* Fully functional 2D Panel Support throughout the CM.
 
* 3D Virtual Cockpit (nonfunctional at the moment)
 
* 3D Virtual Cockpit (nonfunctional at the moment)
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* Realistic simulation of most major spacecraft systems.
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* Full Realism Simulation of most major spacecraft systems.
 
* Historically accurate checklists.
 
* Historically accurate checklists.
 
* NEW CM, SM, and KSC meshes (VAB,LUT,LC34/37/39,MSS,MLP,Crawler etc.)
 
* NEW CM, SM, and KSC meshes (VAB,LUT,LC34/37/39,MSS,MLP,Crawler etc.)
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* Integrated Virtual AGC.
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* Integrated VirtualAGC.
 
* Full launch and landing autopilot for the LEM, and enhanced autopilot for the Saturns and CSM.
 
* Full launch and landing autopilot for the LEM, and enhanced autopilot for the Saturns and CSM.
 
* Meshland integration.
 
* Meshland integration.
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* Engineering camera views during launch.
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* Realism settings to accomidate orbinauts from 9 to 92!
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* Realism settings to accomodate orbinauts from 9 to 92!
 
 
* Support for low-res Saturn 1b and Saturn V meshes as well as high-res.
 
* Support for low-res Saturn 1b and Saturn V meshes as well as high-res.
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* Partial Apollo 5 (unmanned LEM test) support.
 
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* Service Module breaks up on re-entry, based on re-entry heating.
 
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* Apollo 13 oxygen venting simulation.
 
  
 
...and MORE!
 
...and MORE!
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==Supported Spacecraft==
 
==Supported Spacecraft==
  
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Project Apollo for Orbiter 1.0/NASSP 7.0 supports a number of spacecraft. Most are historical spacecraft used in the Apollo program, but some are proposed post-Apollo designs which never flew in the real world.
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NASSP 7.0 supports a number of spacecraft.
  
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===Command and service module===
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==='Apollo to Venus' Wet Workshop test===
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[[Image:NASSP7CSMInOrbitSmall.jpg|thumb|right|NASSP 7.0 CSM in Earth orbit]]
 
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NASSP simulates the Block II Command and service module, providing a home and life support for the astronauts in space.
 
  
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The CM was the nerve center of the Apollo spacecraft, as it functioned as primary control and navigation platform during the missions.  It housed the highly-advanced (for the 1960s) Apollo Guidance Computer, as well as all the systems the astronauts would need to safely re-enter earth's atmosphere.
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[[Image:Apollo-eyeballs-out.jpg|thumb|right|'Wet Workshop' test SIVB burn]]
  
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The Service Module contained the systems that were vital for the extended stay of up to 10 days in space. This included fuel cells to provide power and water, as well as radiators to keep the internal systems cool. Also housed in the service module were the primary propulsion systems, including the RCS maneuverability thrusters and the SPS, used for major course corrections. In later Apollo lunar missions, this versatile component contained a SIM Bay for the additional scientific study of the lunar surface the space surrounding our nearest celestial neighbor.
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NASA's Manned Venus Flyby plans using Apollo technology would have used an SIVB stage to launch a three-man crew towards Venus, after which they would vent remaining fuel from the SIVB, extend solar panels and live in it as a Skylab-style space station. They would conduct generalised astronomical and zero-gravity experiments for most of their trip, and for a few days around the flyby they would conduct detailed observations of Venus.
  
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As the core of the Apollo hardware, the CSM is a high priority for NASSP development. It has received a complete and ongoing overhaul for NASSP 7.0, complete with new graphics, meshes, and systems simulations.
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NASSP 7.0 includes a simulation of the first test phase, in which the astronauts would use the SIVB to raise their orbit for a test of the 'wet workshop' of up to one month in duration. Rather than solar panels, the test phase uses batteries in the SIVB stage to provide power to supplement the Service Module fuel cells and conserve consumables in the Service Module for the return to Earth.
  
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===Lunar Module===
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===ASTP Docking Module===
  
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The Lunar Module was a two-stage lander used to land astronauts on the Moon and return them to orbit.
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Although rather limited as a spacecraft in its own right, the Apollo-Soyuz Test Program Docking Module allows an Apollo Command/Service Module to dock with a Russian Soyuz spacecraft in orbit, and transfer crew between them.
  
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[[Image:NASSP7LEMOnMoonSmall.jpg|thumb|right|NASSP 7.0 LEM on the Moon]]
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The Docking Module is carried into orbit as cargo on a Saturn 1b, in the same way that the Lunar Module is carried as cargo on a Saturn V.
  
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The lower Descent Stage carried the large Descent Engine, fuel for the landing, and batteries and supplies required for the stay on the Moon. It also carried a limited amount of cargo, including, on the later flights, the Lunar Rover. Its final role was to act as a launch pad for the Ascent Stage when the lunar landing phase was complete and they flew back to dock with the CSM in orbit.
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===Command/Service Module===
  
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The upper Ascent Stage provided living quarters for the crew while on the Moon, controls for the landing and ascent, and the smaller Ascent Engine and fuel to carry them into orbit. The Ascent Stage could dock with the CSM itself, but in normal circumstances the docking was flown by the more maneuvrable CSM.
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NASSP simulates the Block II Command/Service Module, providing a home and life support for the astronauts in space.
  
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Whereas the CSM was the brain and body, the LM was the heart of the Apollo Program.  A high priority has been placed on the development of the LM for NASSP.  It is currently in line for new graphics and meshes.  Work is already underway on its internal systems.
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===Lunar Module===
  
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===Lunar Rover===
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The Lunar Module was a two-stage lander used to land astronauts on the Moon and return them to orbit.
  
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[[Image:NASSP7LRVOnMoon.jpg|thumb|right|Driving the NASSP 7.0 Lunar Rover]]
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The lower Descent Stage carried the large Descent Engine, fuel for the landing, and batteries and supplies required for the stay on the Moon. It also carried a limited amount of cargo, including, on the later flights, the Lunar Rover. It's final role was to act as a launch pad for the Ascent Stage when the lunar landing phase was complete and they flew back to dock with the CSM in orbit.
  
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The Lunar Rover was a battery-driven electrically-powered vehicle used by the astronauts to drive around the lunar surface. While hardly a Ferrari, it allowed the astronauts to travel longer distances much faster than they could on foot.
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The upper Ascent Stage provided living quarters for the crew while on the Moon, controls for the landing and ascent, and the smaller Ascent Engine and fuel to carry them into orbit. The Ascent Stage could dock with the CSM itself, but in normal circumstances the docking was flown by the more maneuvrable CSM.
  
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The LRV was folded up in the side of the LEM during the flight, and removed and assembled by the astronauts after landing on the lunar surface. When the lunar exploration was complete, the LRV camera was also used to film the launch of the LEM Ascent Stage carrying the astronauts back to the CSM (though this isn't currently simulated in NASSP).
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===Lunar Rover===
  
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NASSP's LRV has been overhauled with the inclusion of a VC mesh and several working instruments. New animations and more realistic hardware simulation (e.g. power usage for the batteries) are on the drawing board.
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Electrically-powered rover used by the astronauts to drive around the lunar surface.
  
 
===Saturn V===
 
===Saturn V===
  
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The three-stage launcher used to launch command and service module and Lunar Module towards the Moon. This was used to launch Apollos 8 through 17. It is arguably the most powerful rocket ever flown into space.
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Three-stage launcher used to launch a Command/Service Module and Lunar Module towards the Moon. This was used to launch Apollos 8 to 17.
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The Saturn V in NASSP is a highly detailed and increasingly more realistic machine.  Current development is minimal, as it has already reached a high level of detail and accuracy.
 
−
 
 
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===Saturn IB===
 
−
 
 
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The two-stage launcher used to launch a Command/Service Module into Earth orbit. This was used for Apollo 7, the Skylab flights, and the Apollo-Soyuz Test Project flight.  Recent studies have shown that the Saturn IB may have been one of the most cost-effective boosters in lbs per dollar.
 
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Like the Saturn V, NASSP's Saturn IB is highly detailed and extremely accurate.  As a result, it is not a high priority at this time.
 
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===ASTP Docking Module===
 
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Although rather limited as a spacecraft in its own right, the Apollo-Soyuz Test Program Docking Module allows an Apollo command and service module to dock with a Russian Soyuz spacecraft in orbit and transfer crew between them.  The Docking Module is carried into orbit as cargo on a Saturn 1B, in the same way, that the Lunar Module is carried as cargo on a Saturn V.
 
−
 
 
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Development on the Docking Module is currently stalled as work proceeds on higher-priority items, however, it is open to further development and will more likely than not see its share of upgrades.
 
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==='Apollo to Venus' Wet Workshop test===
 
−
 
 
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[[Image:Apollo-eyeballs-out.jpg|thumb|right|'Wet Workshop' test SIVB burn]]
 
  
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NASA's Manned Venus Flyby plans using Apollo technology would have used an SIVB stage to launch a three-man crew towards Venus, after which they would vent remaining fuel from the SIVB, extend solar panels, and live in it as a Skylab-style space station. They would conduct generalized astronomical and zero-gravity experiments for most of their trip, and for a few days around the flyby, they would conduct detailed observations of Venus.
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===Saturn 1b===
  
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NASSP 7.0 includes a simulation of the first test phase, in which the astronauts would use the SIVB to raise their orbit for a test of the 'wet workshop' of up to one month in duration. Rather than solar panels, the test phase uses batteries in the SIVB stage to provide power to supplement the Service Module fuel cells and conserve consumables in the Service Module for the return to Earth.
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Two-stage launcher used to launch a Command/Service Module into Earth orbit. This was used for Apollo 7, the Skylab flights, and the Apollo-Soyuz Test Project flight.
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Although not a historically real mission, this proposal from the Apollo Applications Program is an intriguing and exciting 'fictional' mission.  NASSP is developing this capability both as a historical curiosity and as research/exploration into the feasibility of such a concept.
 
  
 
===Saturn INT-20===
 
===Saturn INT-20===
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[[Image:INT-20-first-stage.jpg|thumb|right|Saturn INT-20]]
 
[[Image:INT-20-first-stage.jpg|thumb|right|Saturn INT-20]]
  
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The two-stage launcher used in a similar manner to the Saturn 1b to launch a Command/Service Module and larger payload into Earth orbit: essentially a cut-down Saturn V with no second stage, mounting an SIVB stage directly on top of the S1C first stage. The S1C also had one engine removed, as the five-engine stage produced too much thrust and would have caused problems with excessive dynamic pressure during launch.
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Two-stage launcher used in a similar manner to the Saturn 1b to launch a Command/Service Module and larger payload into Earth orbit: essentially a cut-down Saturn V with no second stage, mounting an SIVB stage directly on top of the S1C first stage. The S1C also had one engine removed, as the five-engine stage produced too much thrust and would have caused problems with excessive dynamic pressure during launch.
  
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The primary benefit of the INT-20 was a payload capacity about half-way between the Saturn 1b and Saturn V without the cost of creating a new launcher from scratch: the stages were close enough in design that they could be built on the same production line as the Saturn V stages. A three-engine version with a lower payload was also studied but isn't simulated in NASSP.
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The primary benefit of the INT-20 was that it could provide a payload capacity about half-way between the Saturn 1b and Saturn V without the cost of creating a new launcher from scratch: the stages were close enough in design that they could be built on the same production line as the Saturn V stages.
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Another non-historic craft, the INT-20 showed much promise on the drawing board and NASSP hopes to bring such promise to live in the virtual world.
 
  
 
==Future spacecraft==
 
==Future spacecraft==
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Phase C of the Apollo to Venus plan would use an improved version of the 'wet workshop' SIVB with a Block-IV CSM to perform the actual Venus flyby.
 
Phase C of the Apollo to Venus plan would use an improved version of the 'wet workshop' SIVB with a Block-IV CSM to perform the actual Venus flyby.
  
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[http://en.wikipedia.org/wiki/Manned_Venus_Flyby Wikipedia] has some more information.
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===Command/Service Module===
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===Command and service module===
 
  
 
Support may be added for the proposed Block-III CSM with batteries for power in place of fuel cells, and the Block-IV CSM with batteries for power and LEM engines in place of the SPS.
 
Support may be added for the proposed Block-III CSM with batteries for power in place of fuel cells, and the Block-IV CSM with batteries for power and LEM engines in place of the SPS.
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In addition, the inclusion of a Block-I CSM in future versions has been discussed.
 
  
 
===Long-Range Flyer/Lunar Escape System===
 
===Long-Range Flyer/Lunar Escape System===
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Simple two-man rocket using fuel from the LEM. This could be used for scouting missions to sites up to around 50 miles from the main landing site, or, in an emergency, to carry two astronauts from the lunar surface to rendevouz with the CSM.
 
Simple two-man rocket using fuel from the LEM. This could be used for scouting missions to sites up to around 50 miles from the main landing site, or, in an emergency, to carry two astronauts from the lunar surface to rendevouz with the CSM.
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See the [http://en.wikipedia.org/wiki/Lunar_Escape_Systems Wikipedia article] for more information.
 
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===Lunar Motorbike===
 
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Designed as a backup to the Lunar Rover. See [http://www.hq.nasa.gov/office/pao/History/alsj/misc/apmisc-S69-41519.jpg NASA image].
 
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===Original Saturn plans===
 
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The original Saturn-A, -B, -C, and Nova designs, possibly including the earlier lunar landing plans based on multiple launches, or the single launch putting the entire CSM onto the Moon using the massive [http://www.astronautix.com/lvs/saturnc8.htm Saturn C-8] booster.
 
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For more information see, for example, [http://www.astronautix.com/lvfam/saturnc.htm Saturn-C family] and [http://www.astronautix.com/lvfam/nova.htm Nova family] at Astronautix.com.
 
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===Project Able LEM===
 
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A plan to use a mirror in space to light up parts of the Vietnam jungle at night. A modified LEM with a huge flexible mirror attached would be launched into space where the mirror would unfold.
 
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A similar plan proposed using a modified LEM to fly to Soviet satellites and spray paint over their sensors: effectively the first space vandals.
 
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===Project Icarus===
 
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Proposal to divert or destroy an incoming asteroid by launching 100 Megaton nuclear bombs on Saturn Vs.
 
  
 
===Saturn 1===
 
===Saturn 1===
  
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The Saturn 1 was the precursor to the Saturn 1B, using an SIV stage in place of the SIVB. The SIV was smaller, with a lower fuel capacity, and used multiple RL10 engines in place of the J2 engine on the SIVB.
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The Saturn 1 was the precursor to the Saturn 1b, using an SIV stage in place of the SIVB. The SIV was smaller, with a lower fuel capacity, and used multiple RL10 engines in place of the J2 engine on the SIVB.
  
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===Saturn 1B MLV===
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===Saturn 1b MLV===
  
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As part of NASA's cost-cutting plans, they studied a derivative of the Saturn 1b which would replace the S1B stage with a solid rocket similar in size to a shuttle SRB. In essence, this was a 1960s version of NASA's new 'Stick' launcher for the CEV.
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As part of NASA's cost-cutting plans, they studied a derivative of the Saturn 1b which would replace the S1B stage with a solid rocket similar in size to a shuttle SRB. In essence this was a 1960s version of NASA's new 'Stick' launcher for the CEV.
  
 
===Saturn INT-21===
 
===Saturn INT-21===
  
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The two-stage launcher used to launch large payloads into Earth orbit. This was used for the Skylab mission.
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Two-stage launcher used to launch large payloads into Earth orbit. This was used for the Skylab mission.
−
 
 
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===Saturn S-ID stage===
 
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A modified S1C stage which dropped the outer four engines in a similar manner to the Altas dropping two of its engines during launch. As well as multi-stage launchers with greater payloads, it could carry 50,000 pounds to low orbit itself with no second stage.
 
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===Saturn V-24===
 
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Saturn V with stretched stages, new toriodal aerospike engines on the upper stages, uprated F-1 engines on the first stage, and four strap-on boosters with two F-1 engines each. Capable of putting over 500,000 pounds of payload into low Earth orbit.
 
  
 
===Skylab===
 
===Skylab===
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==Comparative screenshots==
 
==Comparative screenshots==
  
−
NASSP has changed significantly over the years, as models, textures, and control panels were updated; historical accuracy was improved, and new special effects were added. NASSP 5.x screenshots are currently missing as it won't run as released under Orbiter 2006.
+
NASSP has changed significantly over the years, as models, textures and control panels were updated, historical accuracy was improved and new special effects were added.
  
 
{| border="1" cellpadding="1"
 
{| border="1" cellpadding="1"
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  |<center>''NASSP 7(beta) Tower Seperation''</center>
 
  |<center>''NASSP 7(beta) Tower Seperation''</center>
 
  |<center>''NASSP 7(beta) SM Breakup''</center>
 
  |<center>''NASSP 7(beta) SM Breakup''</center>
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|-
 
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|[[Image:NASSP7-staging2.jpg|center|160px|NASSP 7(beta) SIC/SII staging]]
 
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|[[Image:NASSP7-CSMDockedWithSIVBSmall.jpg|center|160px|NASSP 7.0 CSM docked with LEM and SIVB]]
 
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|[[Image:NASSP7-Apollo5LaunchSmall.jpg|center|160px|NASSP 7.0 Apollo 5 launch]]
 
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|-
 
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|<center>''NASSP 7(beta) SIC/SII staging''</center>
 
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|<center>''NASSP 7.0 CSM docked with LEM and SIVB''</center>
 
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|<center>''NASSP 7.0 Apollo 5 launch''</center>
 
 
|}
 
|}
  
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* ''[http://www.hq.nasa.gov/office/pao/History/alsj/a15/A15Delco.pdf Apollo 15 Delco manual for AGC]''
 
* ''[http://www.hq.nasa.gov/office/pao/History/alsj/a15/A15Delco.pdf Apollo 15 Delco manual for AGC]''
 
* ''Apollo By The Numbers: A Statistical Reference.'' [http://history.nasa.gov/SP-4029/Apollo_00_Welcome.htm HTML] or [http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20010008244_2001006037.pdf PDF]  
 
* ''Apollo By The Numbers: A Statistical Reference.'' [http://history.nasa.gov/SP-4029/Apollo_00_Welcome.htm HTML] or [http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20010008244_2001006037.pdf PDF]  
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*''[http://history.nasa.gov/afj/aohindex.htm Apollo Operations Handbook-Block II: Vol 1, 1969]''
 
 
*''[http://www.astronautix.com/data/satvint.pdf Final Report - Studies of Improved Saturn V Vehicles and Intermediate Payload Vehicles]''
 
*''[http://www.astronautix.com/data/satvint.pdf Final Report - Studies of Improved Saturn V Vehicles and Intermediate Payload Vehicles]''
 
* ''[http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19790072165_1979072165.pdf Manned Venus Flyby study]'', Feb. 1, 1967
 
* ''[http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19790072165_1979072165.pdf Manned Venus Flyby study]'', Feb. 1, 1967
 
* NASA Marshall Spaceflight Center, ''[http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19740021163_1974021163.pdf Skylab Saturn IB Flight Manual]'', 30th September 1972
 
* NASA Marshall Spaceflight Center, ''[http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19740021163_1974021163.pdf Skylab Saturn IB Flight Manual]'', 30th September 1972
 
*''[http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19750063889_1975063889.pdf Saturn V Flight Manual - SA-503]''
 
*''[http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19750063889_1975063889.pdf Saturn V Flight Manual - SA-503]''
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==See also==
 
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* [[AMSO]]
 
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* [[Saturn V]]
 
  
 
==External links==
 
==External links==
  
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* [http://nassp.sourceforge.net/ Main page at Sourceforge ]
+
* [http://nassp.sourceforge.net/ Main page at Sourceforce ]
 
* [http://spacebarjoe.free.fr/ NASSP 4]
 
* [http://spacebarjoe.free.fr/ NASSP 4]
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** [http://orbit.m6.net/v2/read.asp?id=7739 NASSP 4 release thread]
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:* [http://orbit.m6.net/v2/read.asp?id=7739 NASSP 4 release thread]
 
* [http://www.ibiblio.org/apollo/index.html Virtual AGC]
 
* [http://www.ibiblio.org/apollo/index.html Virtual AGC]
 
* [http://taoyue.com/explore/orbiter.html Landing on the Moon]
 
* [http://taoyue.com/explore/orbiter.html Landing on the Moon]
  
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{{HasPrecis}}
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[[Category:Addons]]
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[[Category:Vessel addons]]
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[[Category: Articles]]
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[[category:realistic addons]]
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[[Category:Orbiter 2010 add-ons]]
 
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[[Category:Orbiter Beta add-ons]]
 
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[[Category:Vessel add-ons]]
 
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[[category:Realistic add-ons]]
 
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[[Category:Historical]]
 

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