Where Flight Simulation Enthusiasts Gather from Around the World!
Category: Orbiter - Spaceships | |
F-4 Phantom |
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File Description:
Take off in the F-4 Phantom from KSC Airport...Press K to lower Hook..Press L-Shift and 1 on NumPad to close the Wingtips..Press L-Shift and 0 on NumPad for Flaps..Press G to raise your gear and press + and CTRL to engage your thrust.....Move mouse while holding right button to look around Virtual Cockpit.....Has animated control surfaces (Elevator,Rudder and Ailerons and Flaps), engine smoke and cockpit.. Uses Vinka's new Spacecraft2.DLL.(included)..) and for the Aircraft.DLL version (Take off in the F-4 Phantom from KSC Airport using Aircraft.DLL...Press K to lower Hook...Press F for Flaps in 10'..Press G to raise your gear and press + and CTRL to engage your thrust..... uses Russell Smith's (MaverickTech's) Aircraft.DLL ((included)) ..the Spacecraft2.DLL version has smoke and sounds (needs OrbiterSound 3.0 or higher installed).Unzip into your Orbiter folder.(Make sure - Use Folder names is ticked when using winzip.)
Filename: | F4_Phantom.zip |
License: | Freeware |
Added: | 9th November 2005, 18:09:44 |
Downloads: | 443 |
Author: | Kev Shanow |
Size: | 944.68 KB |
Category: Orbiter - Miscellaneous Files | |
Advanced Fuel System |
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File Description:
Complete and integrated fuel system for Orbiter spacefract. For use in refueling/defueling operations as well as internal fuel transfers in orbit.
Indludes: Two fuel transfer pumps complete with spool times, governors, safety trips, pump temperature, and qusi-realistic fluid physics for static and dynamic pressure in the system. Ability to address up to 10 tanks per vessel with differening transfer rates and fuel temperature. Internal tank-to-tank transfers and refueling/defueling to and from remote tanks on docked ships. Transfer manifold for filling or refueling multiple tanks at the same time. Vessel and MFD independant operation, meaning the system continues to operate weather you're piloting the vessel or have switched to another one. An integraded MFD for controlling the fuel system. A 31-page users manual including detail on pump preformance, a system diagram, and step-by-step example procedures. PDF format with complete bookmarks and embedded cross-references.
This is half a beta at the present. While it gets the job done it's boud to be rough around the edges in some places.
Filename: | fuelsystem.zip |
License: | Freeware |
Added: | 13th March 2005, 02:53:16 |
Downloads: | 3,411 |
Author: | Imaginos |
Size: | 1.29 MB |
Category: Orbiter - Spaceships | |
Stanford Torus Space Colony v1.0 |
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File Description:
What will future space colonization realistically look like? What is it like to approach a rotating station almost 2km in diameter?
The Stanford Torus is based on a design created during a 10 week program in 1975 held at NASA’s Ames Research Center and Stanford University. The project participants considered how to create a practicable permanent colony in space using existing technology at minimum cost.
The habitat is over 1800m in diameter and spins at 1 rpm to provide 1g of pseudo-gravity.
Package includes a scenario to fly from the ISS up to a GEO rendez-vous with Stanford, as well as documentation on the station itself. I am looking for a texture artist to do the station justice, since my textures are pretty sad. Please contact me at [email protected] if you are interested.
INSTALLATION: You need Vinka's spacecraft.dll to use this add-on. A link is provided in the documentation.
1. Unzip files into your Orbiter directory, preserving the directory structure in the zipfile.
2. Load up the Stanford scenario in the Stanford directory in the Orbiter start window.
3. Enjoy the trip!
Filename: | stanford.zip |
License: | Freeware |
Added: | 25th January 2005, 16:07:13 |
Downloads: | 438 |
Author: | Steven Ouellette |
Size: | 9.44 MB |
Category: Orbiter - Spaceships | |
Stanford Torus Space Colony v1.0 |
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File Description:
What will future space colonization realistically look like? What is it like to approach a rotating station almost 2km in diameter?
The Stanford Torus is based on a design created during a 10 week program in 1975 held at NASA’s Ames Research Center and Stanford University. The project participants considered how to create a practicable permanent colony in space using existing technology at minimum cost.
The habitat is over 1800m in diameter and spins at 1 rpm to provide 1g of pseudo-gravity.
Package includes a scenario to fly from the ISS up to a GEO rendez-vous with Stanford, as well as documentation on the station itself. I am looking for a texture artist to do the station justice, since my textures are pretty sad. Please contact me at [email protected] if you are interested.
INSTALLATION: You need Vinka's spacecraft.dll to use this add-on. A link is provided in the documentation.
1. Unzip files into your Orbiter directory, preserving the directory structure in the zipfile.
2. Load up the Stanford scenario in the Stanford directory in the Orbiter start window.
3. Enjoy the trip!
Filename: | Stanford_Torus_Space_Colony_v10.zip |
License: | Freeware |
Added: | 26th January 2005, 14:32:11 |
Downloads: | 370 |
Author: | Steven Ouellette |
Size: | 2.07 MB |
Category: Orbiter - Spaceships | |
U.S.S. Enterprise 2702-D |
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File Description:
The U.S.S. Enterprise NCC-1701-D was a Galaxy-class extended-duration starship and the flagship of Starfleet. The fifth starship to be named Enterprise, she was commanded by Captain Jean-Luc Picard. With a total of 42 decks, the U.S.S. Enterprise-D was twice the length and had eight times the interior space of the Constitution-class ships of over a century earlier; she carried a combined crew and passenger load of about 1,012.
Defensive systems included 10 phaser banks, 250 photon torpedoes, and a high capacity shield grid; there are some 4,000 power systems in all aboard ship.
Full acceleration time from reverse, sub-light impulse through nominal top warp speed, warp 9, was 0.03 milliseconds. The ship achieved maximum speed of warp 9.5 maximum when pursued by the entity known as "Q"; at warp 9.3 its engines had passed the red line.
By stardate 43205, she had already logged tens of thousands of light-years since setting out around stardate 41153.7 after Jean-Luc Picard formally became her first captain on stardate 41124.
An average day aboard ship, according to Lieutenant Commander Data, included four birthdays, two personnel transfers, two chess tournaments, a secondary school play, four promotions, the celebration of the Hindu Festival of Lights — and a birth and wedding.
Some 13 planets were represented among the ship's complement as of stardate 44247. During the Borg incursion of 2366, Decks 23-25 were sliced open by the enemy during the final battle over Earth and requiring a refit at Earth Station McKinley which lasted 5-6 weeks.
It was far less damage than the kamikaze warp-driven collision Commander Riker had readied as one last recourse, however. During that refit, the starship received a phaser upgrade as well as damage repair and a dilithium chamber articulation frame. It off-loaded the original three Runabouts and the first arriving officers at Deep Space Nine.
The U.S.S. Enterprise-D was destroyed in 2371 after an attack by renegade Klingons breached her warp core. Although the saucer section separated before the breach, the force of the explosion caused the section to crash on the planet Veridian III. Fortunately, losses were minimal.
Filename: | 1701d.zip |
License: | Freeware |
Added: | 12th July 2004, 04:41:12 |
Downloads: | 2,211 |
Author: | Jim Williams |
Size: | 1.45 MB |
Category: Orbiter - Orbital Stations | |
New Skylab 2, 3 And 4 Mission |
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File Description:
Skylab 2
25 May 1973 13:00 GMT. Duration: 28.03 days. Call Sign: Skylab. Backup
Crew: McCandless, Musgrave, Schweickart. Nation: USA. Agency: NASA.
Launch Site: Cape Canaveral . Launch Complex: LC39B. Launch Vehicle:
Saturn IB . LV Configuration: Saturn IB s/n SA-206. Program: Skylab.
Class: Manned. Type: Lunar spacecraft. Spacecraft: Apollo CSM. Payload
: Apollo CSM 116. Mass: 19,979 kg. Location of Spacecraft: Naval
Aviation Museum, Pensacola, FL. Perigee: 427 km. Apogee: 439 km.
Inclination: 50.0 deg. Period: 93.2 min.
Epic repair mission which brought Skylab into working order. Included
such great moments as Conrad being flung through space by the whiplash
after heaving on the solar wing just as the debris constraining it
gave way; deployment of a lightweight solar shield, developed in
Houston in one week, which brought the temperatures down to tolerable
levels. With this flight US again took manned spaceflight duration
record.
When the meteoroid shield ripped loose, it disturbed the mounting of
workshop solar array "wing" two and caused it to partially deploy.
The exhaust plume of the second stage retro-rockets impacted the
partially deployed solar array and literally blew it into space.
Also, a strap of debris from the meteoroid shield overlapped solar
array "wing" number one such that when the programmed deployment
signal occurred, wing number one was held in a slightly opened
position where it was able to generate virtually no power.
In the meantime, the space station had achieved a near-circular orbit
at the desired altitude of 435 kilometers (270 miles). All other
major functions including payload shroud jettison, deployment of the
Apollo Telescope Mount (Skylab's solar observatory) and its solar
arrays, and pressurization of the space station occurred as planned.
Scientists, engineers, astronauts, and management personnel at the
NASA Marshall Space Flight Center and elsewhere worked throughout
the first ten-day period of Skylab's flight to devise the means for
its rescue. Simultaneously, Skylab--seriously overheating--was
maneuvered through varying nose-up attitudes that would best maintain
an acceptable "holding" condition. Because of the loss of the
meteoroid shield, however, this positioning caused workshop
temperatures to rise to 52 degrees Celsius (126 degrees F). During
that ten-day period and for some time thereafter, the space station
operated on less than half of its designed electrical system, in the
partially nose-up attitudes, was generating power at reduced
efficiency. The optimum condition that maintained the most favorable
balance between Skylab temperatures and its power generation
capability occurred at approximately 50 degrees nose-up.
The crew rendezvoused with Skylab on the fifth orbit. After making
substantial repairs, including deployment of a parasol sunshade which
cooled the inside temperatures to 23.8 degrees C (75 degrees F), by
June 4 the workshop was in full operation. In orbit the crew conducted
solar astronomy and Earth resources experiments, medical studies, and
five student experiments; 404 orbits and 392 experiment hours were
completed; three EVAs totalled six hours, 20 minutes.
Skylab 3
28 July 1973 11:10 GMT. Duration: 59.46 days. Call Sign: Skylab.
Backup Crew: Brand, Lenoir, Lind. Nation: USA. Agency: NASA. Launch
Site: Cape Canaveral . Launch Complex: LC39B. Launch Vehicle: Saturn
IB . LV Configuration: Saturn IB s/n SA-207. Program: Skylab. Class:
Manned. Type: Lunar spacecraft. Spacecraft: Apollo CSM. Payload:
Apollo CSM 117. Mass: 20,121 kg. Location of Spacecraft: NASA Lewis
Research Center, Cleveland, OH. Perigee: 422 km. Apogee: 442 km.
Inclination: 50.0 deg. Period: 93.2 min.
Continued maintenance of the Skylab space station and extensive
scientific and medical experiments. Installed twinpole solar shield
on EVA; performed major inflight maintenance; doubled record for
length of time in space. Completed 858 Earth orbits and 1,081 hours
of solar and Earth experiments; three EVAs totalled 13 hours, 43
minutes.
Skylab4
16 November 1973 14:01 GMT. Duration: 84.05 days. Call Sign: Skylab.
Backup Crew: Brand, Lenoir, Lind. Nation: USA. Agency: NASA. Launch
Site: Cape Canaveral . Launch Complex: LC39B. Launch Vehicle: Saturn
IB . LV Configuration: Saturn IB s/n SA-208. Program: Skylab. Class:
Manned. Type: Lunar spacecraft. Spacecraft: Apollo CSM. Payload:
Apollo CSM 118. Mass: 20,847 kg. Location of Spacecraft: National Air
and Space Museum (Smithsonian Institution), Washington, DC. Perigee:
422 km. Apogee: 437 km. Inclination: 50.0 deg. Period: 93.1 min.
Included observation and photography of Comet Kohoutek among numerous
experiments. Completed 1,214 Earth orbits and four EVAs totalling 22
hours, 13 minutes. Increased manned space flight time record by 50%.
Rebellion by crew against NASA Ground Control overtasking led to none
of the crew ever flying again.
Filename: | skylab_mission.zip |
License: | Freeware |
Added: | 11th January 2003, 16:39:14 |
Downloads: | 1,934 |
Author: | Ronald Dandurand |
Size: | 6 KB |