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! Organization
! Organization
| AMSAT-India, William Leijenaar
| AMSAT-India, William Leijenaar
http://amsatindia.org/
|- style="vertical-align:top;"
|- style="vertical-align:top;"
! Mission Type
! Mission Type
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|- style="vertical-align:top;"
|- style="vertical-align:top;"
! Launch
! Launch
| May 5, 2005 on [[Polar Satellite Launch Vehicle|PSLV]]-C6
| May 5, 2005 on [[PSLV-C6]]
|- style="vertical-align:top;"
|- style="vertical-align:top;"
! Launch site
! Launch site
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|- style="vertical-align:top;"
|- style="vertical-align:top;"
! Mission duration
! Mission duration
| Achieved: 9 Years and 2 Months
| ?
|- style="vertical-align:top;"
|- style="vertical-align:top;"
! [[Mass]]
! [[Mass]]
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|-
|-
! colspan="2" bgcolor="#FFDEAD" align="center" | Orbital elements
! colspan="2" bgcolor="#FFDEAD" align="center" | Orbital elements
|- style="vertical-align:top;"
|- style="vertical-align:top;
! [[Semi-major axis]]
! [[Semi-major axis]]
| 7004.27 km
| 7004.27 km
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|}
|}


'''HAMSAT''' also known as '''HAMSAT INDIA''' and '''VU2SAT''' is a [[Miniaturized satellite|microsatellite]] weighing {{convert|42.5|kg|lb|1}}, providing [[amateur radio satellite]] communications services for Indian and international [[amateur radio operator]]s. This satellite carries the in-orbit designation of VO-52, and is an [[OSCAR]] series satellite.
'''HAMSAT''' also known as '''HAMSAT INDIA''', '''VU2SAT''' and '''VO-52''' is a [[Miniaturized satellite|microsatellite]] weighing {{convert|42.5|kg|lb|1}}, providing [[amateur radio satellite]] communications services for Indian and international [[amateur radio operator]]s. This satellite carries the in-orbit designation of VO-52, and is an [[OSCAR]] series satellite.


==History==
It was launched by [[PSLV]]-C6 on May 5, 2005. The main payload was an [[Indian Remote Sensing satellite]], [[CARTOSAT-1]] weighing {{convert|1560|kg|lb|-1}}. HAMSAT was placed into a polar [[sun synchronous orbit]].
It was launched by [[PSLV-C6]] on May 5, 2005. The main payload was an [[Indian Remote Sensing satellite]], [[CARTOSAT-1]] weighing {{convert|1560|kg|lb|-1}}. HAMSAT was placed into a polar [[Sun-synchronous orbit]].


It carries two [[transponder]]s, one built by William Leijenaar (Call Sign: PE1RAH), a Dutch Radio Amateur and graduate engineering student from the [[Higher Technical Institute]] at [[Venlo]] and the other by enthusiasts at [[ISRO]] (Indian Space Research Organisation).
It carries two [[transponder]]s, one built by William Leijenaar (Call Sign: PE1RAH), a Dutch Radio Amateur and graduate engineering student from the [[Higher Technical Institute]] at [[Venlo]] and the other by Ham enthusiasts with help from the [[ISRO]] (Indian Space Research Organisation).<ref>{{cite web |url=http://www.isro.org/satellites/hamsat.aspx |title=HAMSAT |work=[[ISRO]] |url-status=dead |archive-url=https://web.archive.org/web/20100926103619/http://isro.org/satellites/hamsat.aspx |archive-date=2010-09-26 }}</ref> Each transponder is recognized by its beacon. The Indian transponder has an unmodulated carrier on 145.940&nbsp;MHz. The Dutch transponder is modulated with telemetry information on 145.860&nbsp;MHz. Both are linear transponders offering the CW, SSB and FM modes of amateur radio communication. They operate Mode-B for U-V operation with UHF uplink and VHF downlink.<ref name="spacetoday">{{cite web |url=http://www.spacetoday.org/Satellites/Hamsats/Hamsats2000s.html |title=Amateur Radio Satellites Roar Into The 21st Century - 2005: VuSat-OSCAR 52 HamSat |work = spacetoday.org }}</ref>


The satellite joins many previous satellites in amateur radio service; mostly launched by [[AMSAT]].
The satellite joins many previous satellites in amateur radio service; mostly launched by [[AMSAT]].

HAMSAT VO-52 failed in space on 11 July 2014, while on its 49,675th orbit, due to the failure of onboard lithium-ion batteries that have met their end of life. Although the satellite's systems and sub-systems are working normally as per the latest telemetry received, the onboard computer recurring to "Reset" mode due to the failure of batteries is hindering operation. Hence, it was decided not to expect any more meaningful and reliable services from HAMSAT VO-52. On 21 July 2014, ISRO decommissioned ‘HAMSAT-VO52′ officially.<ref name="amsatuk">{{cite web |url=http://amsat-uk.org/2014/07/21/goodbye-hamsat-vo52-rest-in-peace/ |title=Goodbye HAMSAT-VO52 – Rest In Peace |work=amsat-uk.org|date=21 July 2014 }}</ref><ref name="amsat">{{cite web |url=http://www.amsat.org/?p=2988 |title=VO-52 "Hamsat" end of mission |work=[[AMSAT]] |date=28 June 2017 }}</ref>

HAMSAT VO-52 was designed for one-year mission life, but lasted for almost 10 years. The satellite was designed to be maintenance-free, and autonomous. It was a test bed for many new concepts such as a Bus Management Unit (BMU), lithium-ion-based power system, automatic spin rate control and spin axis orientation control (SAOC) for maintaining the satellite attitude without ground commanding. HAMSAT was known as “OSCAR-52” among Amateur HAM operators, and was popular internationally because of its high-sensitivity receiver and strong transmitter.<ref name="amsatuk"/><ref name="amsat"/>

==Specifications==

*The satellite is spin-stabilized. It spins at about 4&nbsp;RPM.
*UHF uplink and VHF downlink
*Uplink transponder frequency: 435.250&nbsp;MHz
*Downlink transponder frequency: 145.900&nbsp;MHz
*Beacon frequencies: 145.860&nbsp;MHz CW telemetry and 145.936&nbsp;MHz unmodulated carrier
*Transponder bandwidth: 60&nbsp;kHz
*Transmitter output power: 1 watt
*Antennas: VHF and UHF turnstiles
*Communication modes: CW, SSB, FM
*Electrical power: Gallium arsenide solar panels charging a lithium-ion battery
*Onboard computer: MAR 31750 processor in the spacecraft's electronic bus management unit for attitude control, telemetry, telecommand for ground control, sensor and actuator functions.<ref name="spacetoday"/>


==See also==
==See also==
{{Portal|Spaceflight}}
*[[Indian space program]]
*[[Indian space program]]
*[[List of Indian satellites]]
*[[List of Indian satellites]]
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==External links==
==External links==
*[http://www.isro.org/satellites/hamsat.aspx ISRO: HAMSAT]
*[https://web.archive.org/web/20100926103619/http://isro.org/satellites/hamsat.aspx ISRO: HAMSAT]
*[http://www.amsat.org/amsat-new/satellites/sat_summary/hamsat.php AMSAT link]
*[https://web.archive.org/web/20080731141914/http://www.amsat.org/amsat-new/satellites/sat_summary/hamsat.php AMSAT link]
*[http://photos.groups.yahoo.com/group/eu-amsat/lst?.dir=/PE1RAH&.src=gr&.order=&.view=t&.done=http%3a//briefcase.yahoo.com/ Yahoo Groups (Photos and discussion)]


==References==
{{Indian space program}}
{{Reflist}}

{{Indian space programme}}
{{Indian spacecraft}}
{{Orbital launches in 2005}}
{{Orbital launches in 2005}}


{{DEFAULTSORT:Hamsat}}
{{DEFAULTSORT:Hamsat}}
[[Category:Space programme of India]]
[[Category:Communications satellites of India]]
[[Category:Amateur radio satellites]]
[[Category:Amateur radio satellites]]
[[Category:Amateur radio in India]]
[[Category:Amateur radio in India]]
[[Category:Artificial satellites orbiting Earth]]
[[Category:Satellites orbiting Earth]]
[[Category:2005 in spaceflight]]
[[Category:Spacecraft launched in 2005]]
[[Category:Satellites]]
[[Category:2005 in India]]
[[Category:Satellites of India]]


{{Amateur-radio-stub}}
{{India-spacecraft-stub}}

Latest revision as of 17:36, 4 July 2024

HAMSAT
Organization AMSAT-India, William Leijenaar

http://amsatindia.org/

Mission Type Communications
Satellite of Earth
Launch May 5, 2005 on PSLV-C6
Launch site Sriharikota
Mission duration Achieved: 9 Years and 2 Months
Mass 42.5 kg (launch)
Orbital elements
Semi-major axis 7004.27 km
Eccentricity 0.0027
Inclination 97.89 degrees
Orbital Period 97.23 minutes
Right ascension of the ascending node 65.14 degrees
Argument of perigee 222.72 degrees

HAMSAT also known as HAMSAT INDIA, VU2SAT and VO-52 is a microsatellite weighing 42.5 kilograms (93.7 lb), providing amateur radio satellite communications services for Indian and international amateur radio operators. This satellite carries the in-orbit designation of VO-52, and is an OSCAR series satellite.

History

[edit]

It was launched by PSLV-C6 on May 5, 2005. The main payload was an Indian Remote Sensing satellite, CARTOSAT-1 weighing 1,560 kilograms (3,440 lb). HAMSAT was placed into a polar Sun-synchronous orbit.

It carries two transponders, one built by William Leijenaar (Call Sign: PE1RAH), a Dutch Radio Amateur and graduate engineering student from the Higher Technical Institute at Venlo and the other by Ham enthusiasts with help from the ISRO (Indian Space Research Organisation).[1] Each transponder is recognized by its beacon. The Indian transponder has an unmodulated carrier on 145.940 MHz. The Dutch transponder is modulated with telemetry information on 145.860 MHz. Both are linear transponders offering the CW, SSB and FM modes of amateur radio communication. They operate Mode-B for U-V operation with UHF uplink and VHF downlink.[2]

The satellite joins many previous satellites in amateur radio service; mostly launched by AMSAT.

HAMSAT VO-52 failed in space on 11 July 2014, while on its 49,675th orbit, due to the failure of onboard lithium-ion batteries that have met their end of life. Although the satellite's systems and sub-systems are working normally as per the latest telemetry received, the onboard computer recurring to "Reset" mode due to the failure of batteries is hindering operation. Hence, it was decided not to expect any more meaningful and reliable services from HAMSAT VO-52. On 21 July 2014, ISRO decommissioned ‘HAMSAT-VO52′ officially.[3][4]

HAMSAT VO-52 was designed for one-year mission life, but lasted for almost 10 years. The satellite was designed to be maintenance-free, and autonomous. It was a test bed for many new concepts such as a Bus Management Unit (BMU), lithium-ion-based power system, automatic spin rate control and spin axis orientation control (SAOC) for maintaining the satellite attitude without ground commanding. HAMSAT was known as “OSCAR-52” among Amateur HAM operators, and was popular internationally because of its high-sensitivity receiver and strong transmitter.[3][4]

Specifications

[edit]
  • The satellite is spin-stabilized. It spins at about 4 RPM.
  • UHF uplink and VHF downlink
  • Uplink transponder frequency: 435.250 MHz
  • Downlink transponder frequency: 145.900 MHz
  • Beacon frequencies: 145.860 MHz CW telemetry and 145.936 MHz unmodulated carrier
  • Transponder bandwidth: 60 kHz
  • Transmitter output power: 1 watt
  • Antennas: VHF and UHF turnstiles
  • Communication modes: CW, SSB, FM
  • Electrical power: Gallium arsenide solar panels charging a lithium-ion battery
  • Onboard computer: MAR 31750 processor in the spacecraft's electronic bus management unit for attitude control, telemetry, telecommand for ground control, sensor and actuator functions.[2]

See also

[edit]
[edit]

References

[edit]
  1. ^ "HAMSAT". ISRO. Archived from the original on 2010-09-26.
  2. ^ a b "Amateur Radio Satellites Roar Into The 21st Century - 2005: VuSat-OSCAR 52 HamSat". spacetoday.org.
  3. ^ a b "Goodbye HAMSAT-VO52 – Rest In Peace". amsat-uk.org. 21 July 2014.
  4. ^ a b "VO-52 "Hamsat" end of mission". AMSAT. 28 June 2017.