Editing Project Apollo for Orbiter

Jump to navigation Jump to search

Warning: You are not logged in. Your IP address will be publicly visible if you make any edits. If you log in or create an account, your edits will be attributed to your username, along with other benefits.

The edit can be undone. Please check the comparison below to verify that this is what you want to do, and then save the changes below to finish undoing the edit.

Latest revision Your text
Line 1: Line 1:
{{Infobox add-on
+
'''NASA's Apollo Space Simulation Project''' is an [[Addon]] for Orbiter which recreates the [[Apollo]] missions.
| 1 = [https://sourceforge.net/projects/nassp/ SourceForge]
 
| 2 = Team project
 
| 3 = 7.0 (stable), 8.0 (beta)
 
| 4 = Orbiter 2010 (7.0), Orbiter Beta (8.0)
 
}}
 
'''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==
  
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.
+
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.
  
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.
+
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.
  
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.
+
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==
Line 23: Line 17:
 
====Early NASSP====
 
====Early NASSP====
  
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.
+
List To Be Compiled...
  
 
====NASSP 3.x====
 
====NASSP 3.x====
Line 30: Line 24:
 
* Rewritten to use Orbiter docking support.
 
* Rewritten to use Orbiter docking support.
  
NASSP 3.0 still runs under Orbiter 2006, with no modifications required.
+
As a side-note, NASSP 3.0 still runs under Orbiter 2006, with no modifications required.
  
 
====NASSP 4.x====
 
====NASSP 4.x====
Line 59: Line 53:
 
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.
 
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.
  
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.
+
====NASSP 6.x====
 
 
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.
 
 
 
=== NCPP 1.0 ===
 
 
 
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.
 
 
 
* New CSM and LM control panel
 
 
 
====Project Apollo - NASSP 6.x====
 
 
 
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..."
 
 
 
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.
* 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.
* Improved Saturn 1B autopilot.
+
* Improved Saturn 1b autopilot.
* More realistic command module aerodynamics.
 
  
====Project Apollo - NASSP 7.0====
+
====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]]
Line 91: Line 69:
 
* 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)
* Realistic simulation of most major spacecraft systems.
+
* 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.)
* Integrated Virtual AGC.
+
* 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.
Line 100: Line 78:
 
* Realism settings to accomodate orbinauts from 9 to 92!
 
* 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.
* Partial Apollo 5 (unmanned LEM test) support.
 
* Service Module breaks up on re-entry, based on re-entry heating.
 
* Apollo 13 oxygen venting simulation.
 
  
 
...and MORE!
 
...and MORE!
Line 108: Line 83:
 
==Supported Spacecraft==
 
==Supported Spacecraft==
  
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.
+
NASSP 7.0 supports a number of spacecraft.
  
===Command and service module===
+
===Command/Service Module===
[[Image:NASSP7CSMInOrbitSmall.jpg|thumb|right|NASSP 7.0 CSM in Earth orbit]]
 
NASSP simulates the Block II Command and service module, providing a home and life support for the astronauts in space.
 
  
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.
+
NASSP simulates the Block II Command/Service Module, providing a home and life support for the astronauts in space.
  
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.
+
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 Guidence Computer, as well as all the systems the astronauts would need to safely reenter earth's atmosphere.
  
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.
+
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 privide 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 versitile component contained a SIM Bay for additional scientific study of the lunar surface the space surrounding our nearest celestial neighbor.
 +
 
 +
As the core of the Apollo hardware, the CSM is a high priority for NASSP development. It has recieved a complete and ongoing overhaul for NASSP 7.0, complete with new graphics, meshes and systems simulations.
  
 
===Lunar Module===
 
===Lunar Module===
Line 124: Line 99:
 
The Lunar Module was a two-stage lander used to land astronauts on the Moon and return them to orbit.
 
The Lunar Module was a two-stage lander used to land astronauts on the Moon and return them to orbit.
  
[[Image:NASSP7LEMOnMoonSmall.jpg|thumb|right|NASSP 7.0 LEM on the Moon]]
+
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.
 
 
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.
 
  
 
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.
 
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.
Line 134: Line 107:
 
===Lunar Rover===
 
===Lunar Rover===
  
[[Image:NASSP7LRVOnMoon.jpg|thumb|right|Driving the NASSP 7.0 Lunar Rover]]
+
Electrically-powered rover used by the astronauts to drive around the lunar surface.
  
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.
+
NASSP's LRV recently got an overhaul with the inclusion of a VC mesh and new animations are on the drawing board.
 
 
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).
 
 
 
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.
 
  
 
===Saturn V===
 
===Saturn V===
  
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.
+
Three-stage launcher used to launch a Command/Service Module and Lunar Module towards the Moon. This was used to launch Apollo's 8 through 17.  It is arguably the most powerful rocket ever flown into space.
  
 
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.
 
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.
  
===Saturn IB===
+
===Saturn 1b===
  
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.
+
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 1b may have been one of the most cost-effective boosters in lbs per dollar.
  
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.
+
Like the Saturn V, NASSP's Saturn 1b is highly detailed and extremely accurate.  As a result, it is not a high priority at this time.
  
 
===ASTP Docking Module===
 
===ASTP Docking Module===
  
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.
+
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.  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.
  
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.
+
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 it's share of upgrades.
  
 
==='Apollo to Venus' Wet Workshop test===
 
==='Apollo to Venus' Wet Workshop test===
Line 164: Line 133:
 
[[Image:Apollo-eyeballs-out.jpg|thumb|right|'Wet Workshop' test SIVB burn]]
 
[[Image:Apollo-eyeballs-out.jpg|thumb|right|'Wet Workshop' test SIVB burn]]
  
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.
+
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.
  
 
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.
 
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.
Line 174: Line 143:
 
[[Image:INT-20-first-stage.jpg|thumb|right|Saturn INT-20]]
 
[[Image:INT-20-first-stage.jpg|thumb|right|Saturn INT-20]]
  
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.
+
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.
  
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.
+
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.
  
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.
+
Another non-historic craft, the INT-20 showed much promise on the drawing board and NASSP hopes to bring such promise to life in the virtual world.
  
 
==Future spacecraft==
 
==Future spacecraft==
Line 192: Line 161:
 
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.
  
[http://en.wikipedia.org/wiki/Manned_Venus_Flyby Wikipedia] has some more information.
+
===Command/Service Module===
 
 
===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.
Line 205: Line 172:
  
 
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.
 
See the [http://en.wikipedia.org/wiki/Lunar_Escape_Systems Wikipedia article] for more information.
 
  
 
===Lunar Motorbike===
 
===Lunar Motorbike===
  
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].
+
Tentatively planned for Apollo 20. See [http://www.hq.nasa.gov/office/pao/History/alsj/misc/apmisc-S69-41519.jpg NASA image].
 
 
===Original Saturn plans===
 
 
 
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.
 
 
 
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.
 
  
 
===Project Able LEM===
 
===Project Able LEM===
Line 222: Line 181:
 
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.
 
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.
  
A similar plan proposed using a modified LEM to fly to Soviet satellites and spray paint over their sensors: effectively the first space vandals.
+
A similar plan proposed using a modified LEM to fly to Soviet satellites and spray paint over their censors: effectively the first space vandals.
  
 
===Project Icarus===
 
===Project Icarus===
Line 230: Line 189:
 
===Saturn 1===
 
===Saturn 1===
  
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.
+
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.
  
===Saturn 1B MLV===
+
===Saturn 1b MLV===
  
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.
+
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===
  
The two-stage launcher used to launch large payloads into Earth orbit. This was used for the Skylab mission.
+
Two-stage launcher used to launch large payloads into Earth orbit. This was used for the Skylab mission.
  
 
===Saturn S-ID stage===
 
===Saturn S-ID stage===
Line 254: Line 213:
 
==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"
Line 289: Line 248:
 
  |<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>
|-
 
|[[Image:NASSP7-staging2.jpg|center|160px|NASSP 7(beta) SIC/SII staging]]
 
|[[Image:NASSP7-CSMDockedWithSIVBSmall.jpg|center|160px|NASSP 7.0 CSM docked with LEM and SIVB]]
 
|[[Image:NASSP7-Apollo5LaunchSmall.jpg|center|160px|NASSP 7.0 Apollo 5 launch]]
 
|-
 
|<center>''NASSP 7(beta) SIC/SII staging''</center>
 
|<center>''NASSP 7.0 CSM docked with LEM and SIVB''</center>
 
|<center>''NASSP 7.0 Apollo 5 launch''</center>
 
 
|}
 
|}
  
Line 310: Line 261:
 
* 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]''
 
==See also==
 
 
* [[AMSO]]
 
* [[Saturn V]]
 
  
 
==External links==
 
==External links==
  
* [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]
** [http://orbit.m6.net/v2/read.asp?id=7739 NASSP 4 release thread]
+
:* [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]
  
{{HasPrecis}}
+
[[Category:Addons]]
 
+
[[Category:Vessel addons]]
[[Category: Articles]]
+
[[category:realistic addons]]
[[Category:Orbiter 2010 add-ons]]
 
[[Category:Orbiter Beta add-ons]]
 
[[Category:Vessel add-ons]]
 
[[category:Realistic add-ons]]
 
[[Category:Historical]]
 

Please note that all contributions to OrbiterWiki are considered to be released under the GNU Free Documentation License 1.2 (see OrbiterWiki:Copyrights for details). If you do not want your writing to be edited mercilessly and redistributed at will, then do not submit it here.
You are also promising us that you wrote this yourself, or copied it from a public domain or similar free resource. Do not submit copyrighted work without permission!

To protect the wiki against automated edit spam, we kindly ask you to solve the following hCaptcha:

Cancel Editing help (opens in new window)