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#Post#: 253--------------------------------------------------
Enduranca Space Agency
DIR By: Enduranca
Date: September 6, 2015, 1:29 pm
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HTML http://topnews.in/law/files/esa-35.jpg
Head of Operations: Margaret Hernandez
Headquarters: Wright Federal Air Forces Building, Landfall
Launch Facility: North Columbia Range Facility (Cape
Disappointment)
Mission: To grant the Federation of Enduranca the ability to
venture beyond the planet, and make further inroads into
scientific discovery, as well as learning about our world. The
defense of the nation is also a priority.
Air Force Correspondant: General Tomas Ridgely
Astronauts:
Maj. Peter Tomas
Cmdr. Carlos Baptista
Lt. Sally Dresden
Lt. David Takahashi
Active Spacecraft:
NorthSAT-1 (GEO; weather satellite)
Sagittarius A (SSO; imaging)
Sagittarius B (SSO; imaging, same orbit as Sagitt A)
24x GPS satellites
Starshine, Expedition 1 (LEO; space station, population 3)
[spoiler]
HTML http://www.ninfinger.org/models/vault2013/Shenzou%209%20-%20Tiangong%201/Shenzhou%209%20-%20Tiangong%201%20(b2).jpg[/spoiler]
Soyuz TMA
#Post#: 254--------------------------------------------------
Re: Enduranca Space Agency
DIR By: Enduranca
Date: September 6, 2015, 1:31 pm
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HTML http://i1-news.softpedia-static.com/images/news2/ESA-Posts-Special-Replay-Video-of-First-Vega-Rocket-Launch-2.jpg
Icarus
Height: 30 meters
Diameter: 3 meters
Payload to Low Earth Orbit: 1,450 kg
Mass: 137k Kg
First Stage:
Length
Diameter
Empty mass
Gross mass
Thrust
Specific impulse
Burn time
Fuel
Second Stage:
Length
Diameter
Empty mass
Gross mass
Thrust
Specific impulse
Burn time
Fuel
Third Stage:
Length
Diameter
Empty mass
Gross mass
Thrust
Specific impulse
Burn time
Fuel
Upper Stage - AVUM
Length
Diameter
Empty mass
Gross mass
Engines
Thrust
Specific impulse
Burn time
Fuel
#Post#: 255--------------------------------------------------
Re: Enduranca Space Agency
DIR By: Enduranca
Date: September 6, 2015, 1:32 pm
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[img]
HTML https://nationalpostcom.files.wordpress.com/2014/06/launchspace.jpg?w=620[/img]
Sentry
Height: 50 meters
Diameter: 10.3 meters
Payload to Low Earth Orbit: 7,100 kg
Mass: 305,000 kg
Boosters:
No. boosters
Engines
Thrust
Specific impulse
Burn time
Fuel
First stage:
Engines
Thrust
Specific impulse
Burn time
Fuel
Second stage:
Engines
Thrust
Specific impulse
Burn time
Fuel
Third stage:
Engines
Thrust
Specific impulse
Burn time
Fuel
#Post#: 256--------------------------------------------------
Re: Enduranca Space Agency
DIR By: Enduranca
Date: September 6, 2015, 1:34 pm
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HTML https://upload.wikimedia.org/wikipedia/commons/3/36/Soyuz-TMA_parts.jpg
HTML http://www.keithmcneill.pwp.blueyonder.co.uk/Soyuz%20TMA%20-%20updated%204.jpg
Soyuz
Manned/Unmanned capsule
Capacity: 3
#Post#: 257--------------------------------------------------
Re: Enduranca Space Agency
DIR By: Enduranca
Date: September 6, 2015, 1:35 pm
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*PUBLIC PRESS RELEASE: ESA TO LAND ON COMET*
Margaret Hernandez was seen on a podium, emblazed with the ESA
symbol.
--- Quote ---
> Thank you all for coming. We at the Enduranca Space Agency are
excited to reveal the plan to intercept and land on a comet
approaching our planet. This will be the first time in history
anyone has attempted this.
>
> The spacecraft is being called the REDROVER, and will include
an orbiter and main body, as well as a smaller lander to attach
to the comet.
>
> More details to follow. Thank you, and may the spirits bless
our attempts.
--- End Quote ---
HTML http://www.spaceflightinsider.com/wp-content/uploads/2014/11/67P-Churyumov-Gerasimenko-comet-Rosetta-Philae-lander-European-Space-Agency-ESA-image-posted-on-SpaceFlight-Insider-655x440.jpg
REDROVER
Rapid Extraterrestrial Delivery and Robotic ObserVation
Expedition Recorder
Launch mass
Lander: 100 kg (220 lb)
Dry mass
Payload mass
Lander: 27 kg (60 lb)
Dimensions
Power
The spacecraft is scheduled to be launched via Sentry rocket,
although if ARTEMIS is constructed by launch time, it would be
the primary vehicle. Launch on ARTEMIS would occur at Curiosity
Space Centre, otherwise the North Columbia Launching Range would
host the probe.
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