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| Category: Orbiter - Spaceships | |
| Salyut 4 - Soyuz 17 |
|
File Description:
***REQUIREMENTS***
spacecraft.dll,
launch scenarios require D. Henderson's CVE-lite 'Proton-k' and 'Soyuz-Launchers' (available at orbiterhangar - www.orbithangar.com/searchauth.cfm?search=dh219, and sourceforge - sourceforge.net/project/showfiles.php?group_id=58685)
***INSTALLATION***
unzip with full paths option to orbiter's root folder.
***USE***
on orbit, jettison each craft to it's on-orbit configuration (sorry, no animations yet...) with the 'j' key (make sure to press 'j' only once with the soyuz or else you'll endup separating the orbital module... doh!!)
'j' key also jettisons the soyuz's orbital module (BO) and propulsion module (PAO) from the reentry capsule (SA)...
also, no parachutes yet for the SA (still working out the details and data on that yet), so have fun on reentry as it'll be your last, cosmonaut!
***NOTES***
the soyuz7k-t included is a new (and hopefully improved) version of my previous one; the salyut4 station is all new...
enjoy!
cheers
hc
| Filename: | Salyut_4__Soyuz_17.zip |
| License: | Freeware |
| Added: | 28th January 2006, 04:25:18 |
| Downloads: | 604 |
| Author: | Hans Castorp |
| Size: | 4.2 MB |
| Category: Orbiter - Miscellaneous Files | |
| Advanced Fuel System |
|
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: | Advanced_Fuel_System.zip |
| License: | Freeware |
| Added: | 13th March 2005, 02:53:16 |
| Downloads: | 3,411 |
| Author: | Imaginos |
| Size: | 1.29 MB |
| Category: Orbiter - Miscellaneous Files | |
| Orbiter *.msh File Export / Import Tool for Gmax and 3DSMax v1.2 |
|
File Description:
Version 1.2 of the .msh file export/import tool for gmax and 3DSMax. New in this version:
| Filename: | Orbiter_msh_File_Export__Import_Tool_for_Gmax_and_.zip |
| License: | Freeware |
| Added: | 7th October 2003, 17:58:08 |
| Downloads: | 1,150 |
| Author: | Alexander Blaß |
| Size: | 24.72 KB |
| Category: Orbiter - Spaceships | |
| Lunar Mission Using Nuclear Power |
|
File Description:
This is a Lunar mission using a Shuttle-C unmanned cargo shuttle to deliver a nuclear powered rocket into orbit. A second mission by the Space Shuttle Atlantis delivers the moon lander and one crewman into orbit to dock to the nuclear N.E.R.V.A.-2 booster, which is capable of taking the single man lander to the moon and back to redock to the Atlantis, and land home safe and sound using the Atlantis.
Although the mission is totally my own creation, the machinery was researched and fairly accurate for weights and fuel efficiency. Using nuclear power a lot of payload can be pushed to the moon because it is over twice as strong as conventional rockets. Also, the Shuttle-C was actually in the process of being built by N.A.S.A during the 1990s (I've seen a photo of a partially built vehicle).
The Shuttle-C uses Vinka's multistage, but I have included the minimum files neccessary to make the Shuttle-C fly. You don't need to download anything other than this add-on. If you don't have Vinka's mulitstage, you won't see boosters or tanks after they've been jettisoned, so it would help to have it anyways.
This add-on is compatible with Build 021217 of Orbiter.
| Filename: | Lunar_Mission_Using_Nuclear_Power.zip |
| License: | Freeware |
| Added: | 11th February 2003, 05:48:15 |
| Downloads: | 2,566 |
| Author: | Kyle |
| Size: | 162.26 KB |
| Category: Orbiter - Spaceships | |
| Minuteman II Missile |
|
File Description:
The Minuteman was Americas Third Operational ICBM System. During the Cuban Missile Crisis it was America's "Ace In The Hole". It has been operational at U.S. bases since 1962 reaching a peak of 1,000 missiles.
The Minuteman II program was economically crucial to the development of integrated circuits. It was the first mass-produced system to use a computer constructed from integrated circuits, and used most of the production of such circuits from 1962 through 1967. The other major customer of these circuits was the Apollo Guidance Computer, which had similar weight and ruggedness constraints.
The Orbiter version keeps up with the historical aspect of this horrible weapon. This add-on is created for historical purposes only, and we do not condone using Orbiter to simulate nuclear war. No active Minuteman II missiles currently exist today. The only way to see one now is at a museum or on display at various Air Force bases world wide. This add-on simulates the flight plan and package delivery of a real Minuteman II missile.
The warhead included in this add-on is from the Trinity package created by Dave Rowbothham. The warhead activates at about 4 minutes to impact. It arms at 2000 feet and detonation occurs at 1800 feet.
| Filename: | Minuteman_II_Missile.zip |
| License: | Freeware |
| Added: | 27th September 2004, 16:24:26 |
| Downloads: | 1,380 |
| Author: | Jim Williams |
| Size: | 1.12 MB |
| Category: Orbiter - Spaceships | |
| Project Mercury Addon Enhancement Pack |
|
File Description:
An enhancement package for the Project Mercury addon for Orbiter created by Rob Conley at the Medville Space Center http://home.alltel.net/estar/orbiter.html This enhancement pack contains updates to the REDSTONE, ATLAS rockets and the MERCURY Spacecraft. The REDSTONE texture was hand crafted in MS Paint (believe it or not) using archived pictures of both Freedom-7 and Liberty Bell 7 pre launch pictures as guides. It is now historically accurate, and cleaned up quite a bit. The ATLAS now sports a realistic corrigated booster section (with the texture taken right from a picture of Gordo Coopers pre-launch Atlas) and the upper section now has the frosty look that occured with the Atlas when it was loaded with LOX and fuel, and some historically accurate markings were included. The improvements to the MERCURY CAPSULE are numerous. It sports a real window (texture taken from a close up shot of Friendship-7), more darker exterior color that is more accurate, crisper detail, improved antenna housing and capsule top. Please note that there are TWO versions of the capsule exterior texture included. One called CAPMAIN.DDS sports a realistic name printed on the exterior, not assiciated with any real mission (America 7), and the other texture, CAPMAIN-NOLOGO.DDS, has no logo imprinted. Refer to the README file for instructions on how to change this to the non-logo capsule.
| Filename: | Project_Mercury_Addon_Enhancement_Pack.zip |
| License: | Freeware |
| Added: | 30th November 2003, 23:52:52 |
| Downloads: | 2,752 |
| Author: | Jim Williams |
| Size: | 131.67 KB |
| Category: Orbiter - Spaceships | |
| Pioneer 4 Add-on for Orbiter |
|
File Description:
Pioneer 3 and 4 were early satellites designed to be lofted toward Earth's Moon. They were equipped with Geiger counters to measure radiation in space. Pioneer 3 was launched from Cape Canaveral, Florida, on December 6, 1958.
Because of a slight error in the satellite's velocity and angle after burnout of the Juno II rocket, it did not reach the Moon; instead it achieved a peak altitude of 102,320 kilometers (63,580 miles). The satellite did, however, discover a second radiation belt around Earth during its flight. Pioneer 3 reentered Earth's atmosphere over equatorial Africa a day after launch.
Pioneer 4 was launched March 3, 1959, and successfully passed within 60,000 kilometers (37,300 miles) of the Moon the following day. The satellite was tracked for 82 hours to a distance of 655,000 kilometers (407,000 miles) from Earth, a record at that time. Pioneer 4 is now orbiting the Sun, the first U.S. spacecraft placed in solar orbit.
The Orbiter version will do a little better than get you within 60,000 kilometers like the real one achieved. The flight profile included usually will get you to within 8,000 kilometers, and sometimes, depending on the mood of your copy of Orbiter, may even impact the moon! However since installations may vary, your distance to the moon on arrival, or even impacting the moon, is not guaranteed. Just like the real thing!
| Filename: | Pioneer_4_Addon_for_Orbiter.zip |
| License: | Freeware |
| Added: | 19th October 2004, 19:59:22 |
| Downloads: | 682 |
| Author: | Jim Williams |
| Size: | 530.42 KB |
| Category: Orbiter - Orbital Stations | |
| Skylab 2 Mission |
|
File Description:
The Skylab space station was launched May 14, 1973, from the NASA
Kennedy Space Center by a huge Saturn V launch vehicle, the moon
rocket of the Apollo Space Program. Sixty-three seconds after liftoff,
the meteoroid shield--designed also to shade Skylab's workshop
--deployed inadvertently. It was torn from the space station by
atmospheric drag. This event and its effects started a ten-day period
in which Skylab was beset with problems that had to be conquered
before the space station would be safe and habitable for the three
manned periods of its planned eight-month mission.
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.
| Filename: | Skylab_2_Mission.zip |
| License: | Freeware |
| Added: | 7th January 2003, 04:31:25 |
| Downloads: | 907 |
| Author: | Ronald Dandurand |
| Size: | 3.76 KB |
| Category: Orbiter - Orbital Stations | |
| New Skylab 2, 3 And 4 Mission |
|
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: | New_Skylab_2_3_And_4_Mission.zip |
| License: | Freeware |
| Added: | 11th January 2003, 16:39:14 |
| Downloads: | 1,934 |
| Author: | Ronald Dandurand |
| Size: | 6.06 KB |
| Category: Orbiter - Miscellaneous Files | |
| Gusev Crater Scenery |
|
File Description:
Gusev Crater is an impact crater on Mars that looks as though a lake may have once filled it in the distant past.
Gusev Crater is about 145 km (90 miles) wide. It is located at 14.6° South latitude and 175.3° East longitude, along the boundary between Mars' southern highlands and its lowland northern plains. The crater is about 3,000 km (1,900 miles) southeast of the volcano Elysium Mons. Scientists believe the Gusev Crater was formed by the impact of an asteroid three to four billion years ago.
A valley named Ma'adim Vallis, which is connected to the south side of the crater, looks like it may have been a river channel that poured water into the crater in the past, forming a large lake. If the crater was indeed a lake, scientists expect it to contain layers of sediments as much as 915 meters (3,000 feet) thick that flowed in with the water. There may be other clues to a watery past within the crater, such as deposits of minerals, such as halite and gypsum, that form when water evaporates. Wet environments are the best places to look for life, which is why scientists are so eager to track down places on Mars that were once wet.
On the 3rd of January 2004, MER-A Spirit, one of the two Mars Exploration Rovers (MER) had landed within an 81 km by 12 km (50 by 7 miles) oval near the center of Gusev Crater. Once settled into its new "home", Spirit will begin its mission of exploring for geologic evidence of the presence of water in Gusev Crater's past.
| Filename: | Gusev_Crater_Scenery.zip |
| License: | Freeware |
| Added: | 5th January 2004, 17:56:22 |
| Downloads: | 1,376 |
| Author: | Robert Stettner (Foxtrot) |
| Size: | 378.72 KB |