Gene Nygaard (talk | contribs) lbs>lb, improper precision |
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| station_image_size = |
| station_image_size = |
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| station_image_caption = Artist rendering of ''Genesis I'' |
| station_image_caption = Artist rendering of ''Genesis I'' |
||
| sign = [[North American Aerospace Defense Command|NORAD]] #31789 <br/> IDC #2007-028A <sup>(1)</sup> |
| sign = [[North American Aerospace Defense Command|NORAD]] #31789 <br /> IDC #2007-028A <sup>(1)</sup> |
||
| crew = Unmanned |
| crew = Unmanned |
||
| launch = [[June 28]], [[2007]] <br/> 15:02:00 UTC <sup>(2)</sup> |
| launch = [[June 28]], [[2007]] <br /> 15:02:00 UTC <sup>(2)</sup> |
||
| launch_pad = [[Dombarovskiy]] base, <br/> [[Russia]] <sup>(2)</sup> |
| launch_pad = [[Dombarovskiy]] base, <br /> [[Russia]] <sup>(2)</sup> |
||
| reentry = |
| reentry = |
||
| status = On orbit |
| status = On orbit |
||
| mass = 1,360 [[kilogram|kg]] <br/> (3,000 [[pound (mass)|lb]]) <sup>(3)</sup> |
| mass = 1,360 [[kilogram|kg]] <br /> (3,000 [[pound (mass)|lb]]) <sup>(3)</sup> |
||
| length = 4.4 [[metre|m]] (14.4 [[foot ( |
| length = 4.4 [[metre|m]] (14.4 [[foot (length)|ft]]) <sup>(3)</sup> |
||
| diameter = 2.54 m (8.3 ft) <sup>(3)</sup> |
| diameter = 2.54 m (8.3 ft) <sup>(3)</sup> |
||
| volume = 11.5 [[cubic metre|m³]] (406.1 [[cubic foot|ft³]]) <sup>(3)</sup> |
| volume = 11.5 [[cubic metre|m³]] (406.1 [[cubic foot|ft³]]) <sup>(3)</sup> |
||
| pressure = |
| pressure = 69.6-72.4 [[pascal (unit)|kPa]] <br /> (10.1-10.5 [[pounds per square inch|psi]]) <sup>(4)</sup> |
||
| perigee = 548.0 [[kilometre|km]] ( |
| perigee = 548.0 [[kilometre|km]] <br /> (340.5 [[mile|mi]]) <sup>(1)</sup> |
||
| apogee = 569.0 km ( |
| apogee = 569.0 km <br /> (353.6 mi) <sup>(1)</sup> |
||
| inclination = 64.51 [[degree (angle)|degrees]] <sup>(1)</sup> |
| inclination = 64.51 [[degree (angle)|degrees]] <sup>(1)</sup> |
||
| speed = |
| speed = |
||
| period = 95.8 minutes <sup>(1)</sup> |
| period = 95.8 minutes <sup>(1)</sup> |
||
| orbits_day = 15.03 <sup>(1)</sup> |
| orbits_day = 15.03 <sup>(1)</sup> |
||
| in_orbit = >150 days <sup>( |
| in_orbit = >150 days <sup>(4)</sup> |
||
| orbits = >2, |
| orbits = >2,300 <sup>(4)</sup> |
||
| distance = |
| distance = |
||
| stats_ref = 1<ref name="n2yoG2">{{cite web |url=http://www.n2yo.com/satellite.php?s=31789 |title=Genesis II satellite details |work=N2YO.com |accessdate=2007-11-30}}</ref>, 2<ref name="RSWdnepr2">{{cite web |url=http://www.russianspaceweb.com/dnepr.html |title=Russia launches prototype of a private space station |work=RussianSpaceWeb.com |date=[[2007-06-28]] |accessdate=2007-06-30}}</ref>, 3<ref name="msnbc397">{{cite news |url=http://www.msnbc.msn.com/id/18142397/ |title=Private space station test delayed till May |work=MSNBC |first=Alan |last=Boyle |date=[[2007-04-17]] |accessdate=2007-06-30}}</ref>}} |
| stats_ref = 1<ref name="n2yoG2">{{cite web |url=http://www.n2yo.com/satellite.php?s=31789 |title=Genesis II satellite details |work=N2YO.com |accessdate=2007-11-30}}</ref>, 2<ref name="RSWdnepr2">{{cite web |url=http://www.russianspaceweb.com/dnepr.html |title=Russia launches prototype of a private space station |work=RussianSpaceWeb.com |date=[[2007-06-28]] |accessdate=2007-06-30}}</ref>, 3<ref name="msnbc397">{{cite news |url=http://www.msnbc.msn.com/id/18142397/ |title=Private space station test delayed till May |work=MSNBC |first=Alan |last=Boyle |date=[[2007-04-17]] |accessdate=2007-06-30}}</ref>, 4<ref name="BAperfG2">{{cite web |url=http://www.bigelowaerospace.com/genesis_II/?Performance |title=Genesis II: Performance |work=BigelowAerospace.com |accessdate=2007-12-20}}</ref> |
||
}} |
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'''''Genesis II''''' is the second experimental space habitat designed and built by the private [[United States|American]] firm [[Bigelow Aerospace]], and was launched in 2007. As the second module sent into orbit by the company, this spacecraft builds on the data and experience gleaned from its previously orbited sister-ship ''[[Genesis I (module)|Genesis I]]'' to continue testing the viability of long-term inflatable space structures. Like its sister-ship and other modules being designed by Bigelow Aerospace, this spacecraft is based on the [[NASA]] [[Transhab]] design, which provides increased interior volume and reduced launch diameter along with potentially reduced mass compared to traditional rigid structures. |
'''''Genesis II''''' is the second experimental space habitat designed and built by the private [[United States|American]] firm [[Bigelow Aerospace]], and was launched in 2007. As the second module sent into orbit by the company, this spacecraft builds on the data and experience gleaned from its previously orbited sister-ship ''[[Genesis I (module)|Genesis I]]'' to continue testing the viability of long-term inflatable space structures. Like its sister-ship and other modules being designed by Bigelow Aerospace, this spacecraft is based on the [[NASA]] [[Transhab]] design, which provides increased interior volume and reduced launch diameter along with potentially reduced mass compared to traditional rigid structures. |
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=== Spacecraft history === |
=== Spacecraft history === |
||
<!--As additional material becomes available, place at the bottom of this section in a timeline sequence.--> |
<!--As additional material becomes available, place at the bottom of this section in a timeline sequence.--> |
||
⚫ | ''Genesis II'' was launched on [[28 June]], [[2007]] at 15:02 [[Coordinated Universal Time|UTC]]. As with ''Genesis I'', it was launched aboard an [[ISC Kosmotras]] [[Dnepr rocket]] from [[Dombarovskiy|Dombarovskiy missile base]] near [[Yasny|Yasniy]], [[Russia]]. It successfully reached orbit after separation from the rocket at 15:16 UTC. Due to the mechanics of its orbit, first contact with the craft was established once it passed over [[SpaceQuest, Ltd.]]'s [[Fairfax, Virginia]] receiving station at 22:20 UTC, confirming that it was alive and functioning nominally with power and air pressure at expected levels.<ref name="BAnews070628-1">{{cite news |url=http://www.bigelowaerospace.com/news/?Genesis_II_Calls_Home |title=Genesis II Calls Home, Says It's Doing Fine |work=BigelowAerospace.com |date=[[2007-06-28]] |accessdate=2007-12-20}}</ref><ref name="BAnews070628-2">{{cite news |url=http://www.bigelowaerospace.com/news/?Genesis_II_Launched |title=Genesis II Successfully Launched |work=BigelowAerospace.com |date=[[2007-06-28]] |accessdate=2007-12-20}}</ref> Externally, ''Genesis II'' is identical in size to ''Genesis I''; as such, it is a one-third scale of the full-size ''[[BA 330]]'' model, with on-orbit measurements of 4.4 [[metre|m]] (14.4 [[foot (length)|ft]]) in length and 2.54 m (8.3 ft) in diameter, with an interior habitable volume of 11.5 cubic meters (406.1 cubic feet). As part of its inflatable design, ''Genesis II'' launched with a diameter of 1.6 m (5.25 ft), expanding to its full size after entering orbit.<ref name="BAnews070628-1"/><ref name="space070628">{{cite news |url=http://www.space.com/missionlaunches/070628_genesis2_update.html |title=Bigelow's Second Orbital Module Launches Into Space |work=Space.com |first=Tariq |last=Malik |coauthors=and Leonard David |date=[[2007-06-28]] |accessdate=2007-06-30}}</ref> Within two days of launch, attitude control systems had dampened all rotation and oriented antennae toward Earth.<ref name="BAperfG2" /> |
||
⚫ | Similar to the process endured by Bigelow for ''Genesis I'', transporting ''Genesis II'' to Russia for launch was the end result of nearly a year of regulatory processes due to restrictions imposted by [[International Traffic in Arms Regulations]] (ITAR) and other procedures, both in the United States and abroad. After leaving [[North Las Vegas, Nevada]] in the United States, the spacecraft made a stopover in [[Luxembourg]] before being flown on an [[Antonov An-124]] to [[Orsk]], Russia, and transported over ground to the Dombarovskiy base. ''Genesis II'' made its final move into the Assembly, Integration and Test Building on [[March 29]], [[2007]].<ref name="dispyasny">{{cite web |url=http://www.bigelowaerospace.com/out_there/dispatches_from_yasny.php |title=Dispatches from Yasny |work=BigelowAerospace.com |first=Mike |last=Gold | month=March |year=2007 |accessdate=2007-12-20 |archiveurl=http://web.archive.org/web/20070509003629/http://www.bigelowaerospace.com/out_there/dispatches_from_yasny.php |archivedate=2007-05-09}}</ref> |
||
⚫ | ''Genesis II'' was launched on [[28 June]], [[2007]] at 15:02 [[Coordinated Universal Time|UTC]]. As with ''Genesis I'', it was launched aboard an [[ISC Kosmotras]] [[Dnepr rocket]] from [[Dombarovskiy|Dombarovskiy missile base]] near [[Yasny|Yasniy]], [[Russia]]. It successfully reached orbit after separation from the rocket at 15:16 UTC. Due to the mechanics of its orbit, first contact with the craft was established once it passed over [[SpaceQuest, Ltd.]]'s [[Fairfax, Virginia]] receiving station at 22:20 UTC, confirming that it was alive and functioning nominally with power and air pressure at expected levels.<ref name="BAnews070628-1">{{cite news |url=http://www.bigelowaerospace.com/ |
||
⚫ | Similar to the process endured by Bigelow for ''Genesis I'', transporting ''Genesis II'' to Russia for launch was the end result of nearly a year of regulatory processes due to restrictions imposted by [[International Traffic in Arms Regulations]] (ITAR) and other procedures, both in the United States and abroad. After leaving [[North Las Vegas, Nevada]] in the United States, the spacecraft made a stopover in [[Luxembourg]] before being flown on an [[Antonov An-124]] to [[Orsk]], Russia, and transported over ground to the Dombarovskiy base. ''Genesis II'' made its final move into the Assembly, Integration and Test Building on [[March 29]], [[2007]].<ref name="dispyasny">{{cite web |url=http://www.bigelowaerospace.com/out_there/dispatches_from_yasny.php |title=Dispatches from Yasny |work=BigelowAerospace.com |first=Mike |last=Gold | month=March |year=2007 |accessdate=2007- |
||
Originally slated for a [[August 6]], [[2006]] launch, ISC Kosmotras delayed the launch to [[January 30]], [[2007]] due to the failure of a Dnepr rocket in July 2006. The launch was delayed an additional four times ([[April 1]], [[April 19]], [[April 26]] and [[May 23]]) due to technical and scheduling concerns before its eventual launch on [[June 28]].<ref name="RSWdnepr2"/> |
Originally slated for a [[August 6]], [[2006]] launch, ISC Kosmotras delayed the launch to [[January 30]], [[2007]] due to the failure of a Dnepr rocket in July 2006. The launch was delayed an additional four times ([[April 1]], [[April 19]], [[April 26]] and [[May 23]]) due to technical and scheduling concerns before its eventual launch on [[June 28]].<ref name="RSWdnepr2"/> |
||
On [[December 12]], [[2007]], Bigelow Aerospace provided an update indicating that ''Genesis II'' was in good health. All cameras have been tested and more than 4,000 photographs have been captured. The craft is in a nearly circular orbit with an [[orbital eccentricity|eccentricity]] of 0.028, and having lost only three miles (five km) since launch, current predictions indicate that it will remain in orbit for more than 12 years. Attitude control systems and all eight solar arrays are operational, and no damage to the outer surface of the craft has been observed. Internal pressure was noted as holding between 10.1 and 10.5 [[pounds per square inch|psi]] (69.6 to 72.4 [[pascal (unit)|kPa]]), with the variation caused by ''Genesis II'' moving in and out of sunlight during its orbit.<ref name="BAperfG2" /> |
|||
=== Systems === |
=== Systems === |
||
⚫ | ''Genesis II'' features a number of improvements over the first pathfinder that was launched. In addition to the standard guidance control systems used on ''Genesis I'', it has [[Momentum wheel|reaction wheel]] assemblies and a precision measurement system, which are used to affect the spacecraft's [[rotation]] rate and [[angular momentum]] without expending fuel. It carries 22 cameras—nine more than on ''Genesis I''—for photographing and filming cargo and ship conditions both inside and out. Some of these are on [[wikt:articulation|articulated]] platforms, and one wireless camera will be capable of additional exterior shots. Instead of the single-tank inflation system used on the first craft, ''Genesis II'' employs multiple tanks for added reliability and to allow for more finely-tuned gas control. Additional layers have been added to the outer shield for increased protection and thermal management. Finally, the on-board sensor suite has been enhanced with additional sensors for pressure, temperature, attitude control and radiation detection, which will help determine the impact of the orbital environment on shipboard systems integrity.<ref name="BAdiffII">{{cite web |url=http://www.bigelowaerospace.com/out_there/genesis_II_difference.php |title=''Genesis II'' Different From ''Genesis I'' |work=BigelowAerospace.com |first=Eric |last=Haakonstad |date=[[2007-03-05]] |accessdate=2007-08-04 |archiveurl=http://web.archive.org/web/20070528014400/http://www.bigelowaerospace.com/out_there/genesis_II_difference.php |archivedate=2007-05-28}}</ref> |
||
⚫ | ''Genesis II'' features a number of improvements over the first pathfinder that was launched. In addition to the standard guidance control systems used on ''Genesis I'', it has [[Momentum wheel|reaction wheel]] assemblies and a precision measurement system, which are used to affect the spacecraft's [[rotation]] rate and [[angular momentum]] without expending fuel. It carries 22 cameras—nine more than on ''Genesis I''—for photographing and filming cargo and ship conditions both inside and out. Some of these are on [[wikt:articulation|articulated]] platforms, and one wireless camera will be capable of additional exterior shots. Instead of the single-tank inflation system used on the first craft, ''Genesis II'' employs multiple tanks for added reliability and to allow for more finely-tuned gas control. Additional layers have been added to the outer shield for increased protection and thermal management. Finally, the on-board sensor suite has been enhanced with additional sensors for pressure, temperature, attitude control and radiation detection, which will help determine the impact of the orbital environment on shipboard systems integrity.<ref name="BAdiffII">{{cite web |url=http://www.bigelowaerospace.com/out_there/genesis_II_difference.php |title=''Genesis II'' Different From ''Genesis I'' |work=BigelowAerospace.com |first=Eric |last=Haakonstad |date=[[2007-03-05]] |accessdate=2007-08-04}}</ref> |
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=== Payload === |
=== Payload === |
||
On both the interior and exterior, ''Genesis II'' carries several non-critical systems for scientific, commercial and entertainment purposes. |
On both the interior and exterior, ''Genesis II'' carries several non-critical systems for scientific, commercial and entertainment purposes. |
||
For the science aspect, ''Genesis II'' carries an upgraded version of the original life-sciences module and is colloquially termed "Life in a Box". This module includes habitats for three organisms: the [[Madagascar hissing cockroach]], previously carried aboard ''Genesis I''; the South African flat rock scorpion, ''Hadogenes troglodytes''; and a colony of [[Red harvester ant|seed-harvester ants]], ''Pogonomyrmex californicus'', along with the queen ant for long-term colonization possibilities. This biobox system includes automated food and water delivery systems, and fans keep fresh air available by circulating internal air with that inside the rest of the spacecraft. Sensors and cameras will monitor the health and activities of the biobox inhabitants, and images of the interior are intended for display on Bigelow's website.<ref name="BAlifebox">{{cite news |url=http://www.bigelowaerospace.com/life_death/life_in_a_box.php |title=Life in a Box |work=BigelowAerospace.com |first=Maijinn |last=Chen |accessdate=2007- |
For the science aspect, ''Genesis II'' carries an upgraded version of the original life-sciences module and is colloquially termed "Life in a Box". This module includes habitats for three organisms: the [[Madagascar hissing cockroach]], previously carried aboard ''Genesis I''; the South African flat rock scorpion, ''Hadogenes troglodytes''; and a colony of [[Red harvester ant|seed-harvester ants]], ''Pogonomyrmex californicus'', along with the queen ant for long-term colonization possibilities. This biobox system includes automated food and water delivery systems, and fans keep fresh air available by circulating internal air with that inside the rest of the spacecraft. Sensors and cameras will monitor the health and activities of the biobox inhabitants, and images of the interior are intended for display on Bigelow's website.<ref name="BAlifebox">{{cite news |url=http://www.bigelowaerospace.com/life_death/life_in_a_box.php |title=Life in a Box |work=BigelowAerospace.com |first=Maijinn |last=Chen |accessdate=2007-12-20 |archiveurl=http://web.archive.org/web/20070513040221/http://www.bigelowaerospace.com/life_death/life_in_a_box.php |archivedate=2007-05-13}}</ref> |
||
There are two commercial payloads included on ''Genesis II''. The first is the "Fly Your Stuff" program, which allowed individuals and customers to send photographs and other small items into orbit for a fee. Several dozen of these objects were launched, and were later photographed and filmed by cameras in the spacecraft and posted on the Bigelow website for the customers to view.<ref name="BAflystuff">{{cite web |url=http://www.bigelowaerospace.com/ |
There are two commercial payloads included on ''Genesis II''. The first is the "Fly Your Stuff" program, which allowed individuals and customers to send photographs and other small items into orbit for a fee. Several dozen of these objects were launched, and were later photographed and filmed by cameras in the spacecraft and posted on the Bigelow website for the customers to view.<ref name="BAflystuff">{{cite web |url=http://www.bigelowaerospace.com/image_gallery/?fid=9 |title=Fly Your Stuff |work=BigelowAerospace.com |accessdate=2007-12-20}}</ref> By December 2007, all objects launched as part of this program had been photographed and distributed to customers.<ref name="BAperfG2" /> A secondary payload is the external image projection system that tested the capability for flashing images and messages on the spacecraft's hull. Two projectors and associated cameras are positioned on the tips of solar arrays, and the company has eventual plans for allowing the public to send images and video to be displayed. [[As of August 2007]], there were no firm plans on how this would be handled due to current limits of uplink bandwidth, and was considered an experimental "fun" project.<ref name="msnbc3924">{{cite news |url=http://cosmiclog.msnbc.msn.com/archive/2007/08/03/303924.aspx |title=Orbital Billboard Lights Up |work=MSNBC Cosmic Log |first=Alan |last=Boyle |date=[[2007-08-03]] |accessdate=2007-08-10}}</ref><ref name="space070326">{{cite news |url=http://www.space.com/spacenews/070326_bigelow_businessmonday.html |title=Bigelow Aerospace Sets a Business Trajectory |work=Space.com |first=Leonard |last=David |date=[[2007-03-26]] |accessdate=2007-08-06}}</ref> |
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For entertainment, ''Genesis II'' carries a "Space [[Bingo (U.S.)|Bingo]]" game intended to foster public interest in the program. The game will be started several months into the mission and will be free to play, though there will be no actual gambling involved. The game module contains a full set of Bingo balls which are randomly manipulated one at a time by a system of fans and levers, resetting after forty balls have entered play. During play, images will be broadcast to those who are playing along.<ref name="BAbingo">{{cite news |url=http://www.bigelowaerospace.com/ |
For entertainment, ''Genesis II'' carries a "Space [[Bingo (U.S.)|Bingo]]" game intended to foster public interest in the program. The game will be started several months into the mission and will be free to play, though there will be no actual gambling involved. The game module contains a full set of Bingo balls which are randomly manipulated one at a time by a system of fans and levers, resetting after forty balls have entered play. During play, images will be broadcast to those who are playing along.<ref name="BAbingo">{{cite news |url=http://www.bigelowaerospace.com/games/?Bigelow_Bingo |title=Bigelow Bingo |work=BigelowAerospace.com |first=Maijinn |last=Chen |accessdate=2007-12-20}}</ref> |
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== References == |
== References == |
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[[Category:Private spaceflight]] |
[[Category:Private spaceflight]] |
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[[Category:Space stations]] |
[[Category:Space stations]] |
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[[pl:Genesis II]] |
Revision as of 12:03, 20 December 2007
Station statistics | |
---|---|
COSPAR ID | 2007-028A |
SATCAT no. | 31789 |
Call sign | NORAD #31789 IDC #2007-028A (1) |
Crew | Unmanned |
Launch | June 28, 2007 15:02:00 UTC (2) |
Launch pad | Dombarovskiy base, Russia (2) |
Mission status | On orbit |
Mass | 1,360 kg (3,000 lb) (3) |
Length | 4.4 m (14.4 ft) (3) |
Diameter | 2.54 m (8.3 ft) (3) |
Pressurised volume | 11.5 m³ (406.1 ft³) (3) |
Atmospheric pressure | 69.6-72.4 kPa (10.1-10.5 psi) (4) |
Periapsis altitude | 548.0 km (340.5 mi) (1) |
Apoapsis altitude | 569.0 km (353.6 mi) (1) |
Orbital inclination | 64.51 degrees (1) |
Orbital period | 95.8 minutes (1) |
Orbits per day | 15.03 (1) |
Days in orbit | >150 days (4) |
No. of orbits | >2,300 (4) |
References:1[1], 2[2], 3[3], 4[4] |
Genesis II is the second experimental space habitat designed and built by the private American firm Bigelow Aerospace, and was launched in 2007. As the second module sent into orbit by the company, this spacecraft builds on the data and experience gleaned from its previously orbited sister-ship Genesis I to continue testing the viability of long-term inflatable space structures. Like its sister-ship and other modules being designed by Bigelow Aerospace, this spacecraft is based on the NASA Transhab design, which provides increased interior volume and reduced launch diameter along with potentially reduced mass compared to traditional rigid structures.
Spacecraft history
Genesis II was launched on 28 June, 2007 at 15:02 UTC. As with Genesis I, it was launched aboard an ISC Kosmotras Dnepr rocket from Dombarovskiy missile base near Yasniy, Russia. It successfully reached orbit after separation from the rocket at 15:16 UTC. Due to the mechanics of its orbit, first contact with the craft was established once it passed over SpaceQuest, Ltd.'s Fairfax, Virginia receiving station at 22:20 UTC, confirming that it was alive and functioning nominally with power and air pressure at expected levels.[5][6] Externally, Genesis II is identical in size to Genesis I; as such, it is a one-third scale of the full-size BA 330 model, with on-orbit measurements of 4.4 m (14.4 ft) in length and 2.54 m (8.3 ft) in diameter, with an interior habitable volume of 11.5 cubic meters (406.1 cubic feet). As part of its inflatable design, Genesis II launched with a diameter of 1.6 m (5.25 ft), expanding to its full size after entering orbit.[5][7] Within two days of launch, attitude control systems had dampened all rotation and oriented antennae toward Earth.[4]
Similar to the process endured by Bigelow for Genesis I, transporting Genesis II to Russia for launch was the end result of nearly a year of regulatory processes due to restrictions imposted by International Traffic in Arms Regulations (ITAR) and other procedures, both in the United States and abroad. After leaving North Las Vegas, Nevada in the United States, the spacecraft made a stopover in Luxembourg before being flown on an Antonov An-124 to Orsk, Russia, and transported over ground to the Dombarovskiy base. Genesis II made its final move into the Assembly, Integration and Test Building on March 29, 2007.[8]
Originally slated for a August 6, 2006 launch, ISC Kosmotras delayed the launch to January 30, 2007 due to the failure of a Dnepr rocket in July 2006. The launch was delayed an additional four times (April 1, April 19, April 26 and May 23) due to technical and scheduling concerns before its eventual launch on June 28.[2]
On December 12, 2007, Bigelow Aerospace provided an update indicating that Genesis II was in good health. All cameras have been tested and more than 4,000 photographs have been captured. The craft is in a nearly circular orbit with an eccentricity of 0.028, and having lost only three miles (five km) since launch, current predictions indicate that it will remain in orbit for more than 12 years. Attitude control systems and all eight solar arrays are operational, and no damage to the outer surface of the craft has been observed. Internal pressure was noted as holding between 10.1 and 10.5 psi (69.6 to 72.4 kPa), with the variation caused by Genesis II moving in and out of sunlight during its orbit.[4]
Systems
Genesis II features a number of improvements over the first pathfinder that was launched. In addition to the standard guidance control systems used on Genesis I, it has reaction wheel assemblies and a precision measurement system, which are used to affect the spacecraft's rotation rate and angular momentum without expending fuel. It carries 22 cameras—nine more than on Genesis I—for photographing and filming cargo and ship conditions both inside and out. Some of these are on articulated platforms, and one wireless camera will be capable of additional exterior shots. Instead of the single-tank inflation system used on the first craft, Genesis II employs multiple tanks for added reliability and to allow for more finely-tuned gas control. Additional layers have been added to the outer shield for increased protection and thermal management. Finally, the on-board sensor suite has been enhanced with additional sensors for pressure, temperature, attitude control and radiation detection, which will help determine the impact of the orbital environment on shipboard systems integrity.[9]
Payload
On both the interior and exterior, Genesis II carries several non-critical systems for scientific, commercial and entertainment purposes.
For the science aspect, Genesis II carries an upgraded version of the original life-sciences module and is colloquially termed "Life in a Box". This module includes habitats for three organisms: the Madagascar hissing cockroach, previously carried aboard Genesis I; the South African flat rock scorpion, Hadogenes troglodytes; and a colony of seed-harvester ants, Pogonomyrmex californicus, along with the queen ant for long-term colonization possibilities. This biobox system includes automated food and water delivery systems, and fans keep fresh air available by circulating internal air with that inside the rest of the spacecraft. Sensors and cameras will monitor the health and activities of the biobox inhabitants, and images of the interior are intended for display on Bigelow's website.[10]
There are two commercial payloads included on Genesis II. The first is the "Fly Your Stuff" program, which allowed individuals and customers to send photographs and other small items into orbit for a fee. Several dozen of these objects were launched, and were later photographed and filmed by cameras in the spacecraft and posted on the Bigelow website for the customers to view.[11] By December 2007, all objects launched as part of this program had been photographed and distributed to customers.[4] A secondary payload is the external image projection system that tested the capability for flashing images and messages on the spacecraft's hull. Two projectors and associated cameras are positioned on the tips of solar arrays, and the company has eventual plans for allowing the public to send images and video to be displayed. As of August 2007, there were no firm plans on how this would be handled due to current limits of uplink bandwidth, and was considered an experimental "fun" project.[12][13]
For entertainment, Genesis II carries a "Space Bingo" game intended to foster public interest in the program. The game will be started several months into the mission and will be free to play, though there will be no actual gambling involved. The game module contains a full set of Bingo balls which are randomly manipulated one at a time by a system of fans and levers, resetting after forty balls have entered play. During play, images will be broadcast to those who are playing along.[14]
References
- ^ "Genesis II satellite details". N2YO.com. Retrieved 2007-11-30.
- ^ a b "Russia launches prototype of a private space station". RussianSpaceWeb.com. 2007-06-28. Retrieved 2007-06-30.
{{cite web}}
: Check date values in:|date=
(help) - ^ Boyle, Alan (2007-04-17). "Private space station test delayed till May". MSNBC. Retrieved 2007-06-30.
{{cite news}}
: Check date values in:|date=
(help) - ^ a b c d "Genesis II: Performance". BigelowAerospace.com. Retrieved 2007-12-20.
- ^ a b "Genesis II Calls Home, Says It's Doing Fine". BigelowAerospace.com. 2007-06-28. Retrieved 2007-12-20.
{{cite news}}
: Check date values in:|date=
(help) - ^ "Genesis II Successfully Launched". BigelowAerospace.com. 2007-06-28. Retrieved 2007-12-20.
{{cite news}}
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(help) - ^ Malik, Tariq (2007-06-28). "Bigelow's Second Orbital Module Launches Into Space". Space.com. Retrieved 2007-06-30.
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suggested) (help) - ^ Gold, Mike (2007). "Dispatches from Yasny". BigelowAerospace.com. Archived from the original on 2007-05-09. Retrieved 2007-12-20.
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ignored (help) - ^ Haakonstad, Eric (2007-03-05). "Genesis II Different From Genesis I". BigelowAerospace.com. Archived from the original on 2007-05-28. Retrieved 2007-08-04.
{{cite web}}
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(help) - ^ Chen, Maijinn. "Life in a Box". BigelowAerospace.com. Archived from the original on 2007-05-13. Retrieved 2007-12-20.
- ^ "Fly Your Stuff". BigelowAerospace.com. Retrieved 2007-12-20.
- ^ Boyle, Alan (2007-08-03). "Orbital Billboard Lights Up". MSNBC Cosmic Log. Retrieved 2007-08-10.
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(help) - ^ David, Leonard (2007-03-26). "Bigelow Aerospace Sets a Business Trajectory". Space.com. Retrieved 2007-08-06.
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(help) - ^ Chen, Maijinn. "Bigelow Bingo". BigelowAerospace.com. Retrieved 2007-12-20.
See also