TechEdSat#TechEdSat-6
{{Short description|Space technology development program}}
{{Use American English|date=December 2020}}
{{Use dmy dates|date=December 2020}}
Technology Education Satellite (TechEdSat) is a successful nano-sat flight series conducted from the NASA Ames Research Center in collaboration with numerous universities (San Jose State University, University of Idaho, University of California, University of Minnesota, and Smith College). While one of the principal aims has been to introduce young professionals and university students to the practical realm of developing space flight hardware, considerable innovations have been introduced. In addition, this evolving flight platform has tested concepts for Low Earth Orbit (LEO) sample return, as well as planetary nano-sat class mission concepts.
TechEdSat-1
{{Infobox spaceflight
| name = TechEdSat-1
| names_list = TES-1
| image = TechEdSat.jpg
| image_caption = Computer-aided design drawing of TechEdSat-1
| image_size = 290px
| mission_type = Technology demonstration
| operator = NASA Ames Research Center{{·}}San Jose State University{{·}}University of Idaho{{·}}JAXA{{·}}ÅAC Microtec
| COSPAR_ID = 2012-038D (1998-067CQ) {{cite web|url=https://nssdc.gsfc.nasa.gov/nmc/|title=NASA|website=nssdc.gsfc.nasa.gov|date=14 May 2020|access-date=13 January 2021}} {{PD-notice}}
| SATCAT = 38854
| mission_duration = 213 days (achieved)
100 days (planned)
| spacecraft_type = CubeSat
| spacecraft_bus = CubeSat
| launch_mass = {{cvt|1.2|kg}}
| dimensions = 11.35 cm x 10.0 cm x 10.0 cm (1U)
| power = 1.229 watts
| launch_date = 21 July 2012, 02:06:18 UTC
| launch_rocket = H-IIB F3
| launch_site = Tanegashima Space Center,
Yoshinobu LC-Y2
| launch_contractor = Mitsubishi Heavy Industries
| deployment_from = ISS Kibō
Delivered by Kounotori 3
| deployment_date = 4 October 2012,
15:44:15.297 UTC
| decay_date = 5 May 2013
| orbit_reference = Geocentric orbit
| orbit_regime = Low Earth orbit
| orbit_periapsis = {{cvt|402|km}}
| orbit_apoapsis = {{cvt|422|km}}
| orbit_inclination = 51.66°
| orbit_period = 92.80 minutes
| apsis = gee
}}
File:TechEdSat_Engineering_Development_Unit.jpg
File:TechEdSat Solar Panel.jpg
File:CubeSats launched by ISS Expedition 33.jpg (ISS) on 4 October 2012 (from left: TechEdSat-1, F-1 and FITSAT-1).]]
The first TechEdSat (later renamed "TechEdSat-1" or "TES-1"){{Cite web|url=https://space.skyrocket.de/doc_sdat/techedsat.htm|title=TechEdSat 1 (TES 1)|website=Gunter's Space Page}}{{Cite web|url=https://www.nasa.gov/sites/default/files/atoms/files/techedsat5-factsheet-508-april2017.pdf|title=NASA.gov}} was a 1U-Cubesat designed to evaluate Space Plug-and-play Avionics (SPA) designed in Sweden by ÅAC Microtec. It was also originally intended to perform a communications experiment utilizing the Iridium and Orbcomm satellite phone network,{{cite web |url=http://space.skyrocket.de/doc_sdat/techedsat.htm|title=TechEdSat|last=Gunter|first=Krebs|date=January 31, 2012|publisher=Gunter's Space Page|access-date=13 January 2021}} although this function was disabled before launch.{{cite web|url=https://amsat-uk.org/2012/02/24/techedsat-to-use-satphone/|title=TechEdSat to use SatPhone: The plan to transmit from space using frequencies allocated to Iridium and Orbcomm SatPhone ground stations has been cancelled. A statement from the team says: "We were forced to disable the Iridium modem as our Federal Communications Commission (FCC) license did not come in time. As usual, building the satellite is the easy part".|publisher=AMSAT-UK|date=24 February 2012|access-date=14 January 2021}} TechEdSat was deployed into orbit from the International Space Station (ISS) on 4 October 2012. It reentered to atmosphere on 5 May 2013.{{cite web|url=https://twitter.com/TechEdSat/status/331441656656175104|title=TechEdSat-1|website=twitter.com}}
= Hardware =
- Quake Global Q1000 Modem (Orbcomm) (deactivated) [https://directory.eoportal.org/web/eoportal/satellite-missions/t/techedsat TechEdSat specifications] (accessed 12 September 2014)
- Quake Global Q9602 Modem (Iridium) (deactivated)
- Stensat Radio Beacon
- 4 x nanoRTU (ÅAC Microtec)
- Main Power Distribution Board (ÅAC Microtec)
- RTU Lite (ÅAC Microtec)
- 2 meter band Monopole Antenna
- 70 cm band Monopole Antenna
- 1600 MHz Patch Antenna
- Pumpkin, Inc. 1U Skeletonized CubeSat Structure
- Canon BP-930 Lithium-ion battery
= Specifications =
- Dimensions: 11.35 cm x 10.0 cm x 10.0 cm
- Mass: 1.2 kg (2.6 lb)
- Power Consumption (Safe Mode): 0.350 W
- Power Consumption (Safe Mode, Stensat Transmitting): 3.400 W
- Power Consumption (Nominal Mode): 3.965 W
- Power Consumption (Q1000 Transmitting): 27.125 W
- Power Consumption (Q9602 Transmitting): 10.490 W
- Power Consumption (Nominal Mode, Stensat Transmitting): 7.015 W
- Solar Array (Average): 1.229 W
- Power Storage: 17 Wh
= Launch =
TechEdSat was launched from pad 2 of the Tanegashima Space Center, Yoshinobu Launch Complex (LC-Y2) on 21 July 2012, at 02:06 UTC,{{cite web |url=https://www.nasaspaceflight.com/2012/07/japanese-h-iib-launch-htv-3-international-space-station/|title=Japanese H-IIB launches HTV-3 to the International Space Station|website=nasaspaceflight.com|date=20 July 2012 |access-date=2018-09-08}} aboard Kounotori 3 atop an H-IIB launch vehicle. Kounotori 3 carried the satellite, along with the RAIKO, WE WISH, Niwaka, and F-1 spacecraft, to the International Space Station (ISS), from where it was deployed via the JAXA J-SSOD deployer, from the Kibō module on 4 October 2012 at 15:44:15.297 UTC.{{cite web|url=http://turing.cs.fit.ac.jp/~fitsat/Orbital_Element.txt|title=CubeSat Orbital Elements|archive-url=https://archive.today/20121219061521/http://turing.cs.fit.ac.jp/~fitsat/Orbital_Element.txt|archive-date=December 19, 2012|url-status=dead|access-date=October 4, 2012}}
= Beacon Packet Format =
TechEdSat-1 transmitted a heartbeat packet over amateur radio every 4 seconds. These packets are 122 ASCII character AX.25 packets. Amateur band radio frequency is 437.465 MHz.{{cite web |url=http://www.amsatuk.me.uk/iaru/finished_detail.php?serialnum=228|title=TechEdSat|publisher=IARU|date=April 3, 2012|access-date=April 6, 2012}} Two consecutive 12 bit raw Analog-to-digital converter (ADC) data values are parsed into one 3 byte chunk in order to save data space.
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TechEdSat-2
{{Infobox spaceflight
| name = TechEdSat-2
| names_list = TES-2
PhoneSat v2a
PhoneSat 2.0 Beta
Alexander
| image =
| image_caption =
| image_size = 290px
| mission_type = Technology demonstration
| operator = NASA Ames Research Center
| COSPAR_ID = 2013-016C
| SATCAT = 39144
| mission_duration = 7 days (planned)
6 days (achieved)
| spacecraft_type = CubeSat
| manufacturer = NASA Ames Research Center
| launch_mass = {{cvt|0.5|kg}}
| dimensions = 10 cm x 10 cm x 10 cm (1U)
| power =
| launch_date = 21 April 2013, 21:00:02.2 UTC{{cite web|url=http://www.spaceflight101live.com/live-antares-a-one-mission.html|title=Antares A-ONE Mission Coverage|publisher=Spaceflight101|date=21 April 2013|access-date=6 January 2016|archive-date=15 February 2016|archive-url=https://web.archive.org/web/20160215224940/http://www.spaceflight101live.com/live-antares-a-one-mission.html|url-status=dead}}
| launch_rocket = Antares 110 A-ONE
| launch_site = Wallops Island MARS, LP-0A
| launch_contractor = Orbital Sciences
| deployment_date =
| decay_date = 27 April 2013
| orbit_reference = Geocentric orbit{{cite web|url=http://planet4589.org/space/log/satcat.txt|title=Satellite Catalog|last=McDowell|first=Jonathan|website=Jonathan's Space Report|access-date=8 September 2018}}
| orbit_regime = Low Earth orbit
| orbit_periapsis = {{cvt|218|km}}
| orbit_apoapsis = {{cvt|228|km}}
| orbit_inclination = 51.64°
| orbit_period = 88.95 minutes
| apsis = gee
}}
An Iridium transceiver flew aboard the PhoneSat v2a CubeSat as the TechEdSat-2 mission, separate from the spacecraft originally planned as TechEdSat-2.{{cite web |url=https://space.skyrocket.de/doc_sdat/phonesat-v2.htm|title=PhoneSat 2.0|website=space.skyrocket.de|date=23 September 2019|access-date=12 January 2021}}
Alexander, also known as PhoneSat 2.0 Beta or PhoneSat v2a is a technology demonstration satellite operated by NASA's Ames Research Center, which was launched on 21 April 2013. Part of the PhoneSat programme, it was one of the first three PhoneSat spacecraft, and the first Phonesat-2.0 satellite, to be launched. A PhoneSat-2.0 satellite, Alexander, was built to the single-unit (1U) CubeSat specification, and measures {{cvt|10|cm}} in each dimension. The satellite is based around an off-the-shelf Samsung Electronics Nexus S smartphone which serves in place of an onboard computer. The satellite is equipped with a two-way S-band transponder and solar cells for power generation. The spacecraft uses the phone's gyroscopes, along with a GPS receiver, to determine its position and orientation, and a system of reaction wheels and magnetorquer coils for attitude control.{{cite web |url=https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=2013-016C|title=Alexander 2013-016C|publisher=NASA|date=14 May 2020|access-date=12 January 2021}} {{PD-notice}}
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TechEdSat-3p
{{Infobox spaceflight
| name = TechEdSat-3p
| names_list = TES-3
| image =
| image_caption =
| image_size = 290px
| mission_type = Technology demonstration
| operator = NASA Ames Research Center{{·}}San Jose State University{{·}}University of Idaho{{·}}
| COSPAR_ID = 1998-067DD (TECHEDS3P)
| SATCAT = 39415
| mission_duration = 47 days (achieved)
| spacecraft_type = CubeSat
| launch_mass =
| dimensions = 30 cm x 10 cm x 10 cm (3U)
| power =
| launch_date = 3 August 2013, 19:48:46 UTC
| launch_rocket = H-IIB F4
| launch_site = Tanegashima Space Center,
Yoshinobu LC-Y2
| launch_contractor = Mitsubishi Heavy Industries
| deployment_date = 20 November 2013, 07:58 UTC
| decay_date = 16 January 2014
| orbit_reference = Geocentric orbit
| orbit_regime = Low Earth orbit
| orbit_periapsis = 410 km
| orbit_apoapsis = 415 km
| orbit_inclination = 51.65°
| orbit_period = 92.81 minutes
| apsis = gee
}}
TechEdSat-3p was the third spacecraft flown in the TechEdSat series. Its dimensions were approximately 30 cm x 10 cm x 10 cm, or three CubeSat units long, making it three times larger than TechEdSat-1. TechEdSat-3p was launched to the International Space Station (ISS) on 3 August 2013 from Tanegashima Space Center, Japan on the Kounotori 4 (HTV-4) International Space Station cargo resupply mission and subsequently deployed into orbit by the JEM-Small Satellite Orbital Deployer (J-SSOD).
TechEdSat-3p was the first satellite of the TechEdSat series to include an exo-brake, a parachute-like drag device to demonstrate passive deorbit capability.[http://www.techedsat.co/techedsat3.html] (access-date=12 September 2014) The deployment of an exo-brake increases the surface area of a satellite, increasing its coefficient of drag in the thin upper atmosphere and causing the satellite to deorbit faster than it otherwise would. This technology could be used to more quickly dispose of satellites in Low Earth Orbit that have completed their missions, decreasing the amount of potentially hazardous debris in space. The exo-brake is currently being developed for use as part of the Small Payload Quick Return (SPQR) concept, which would enable science materials to be returned to Earth from the International Space Station whenever is most convenient for scientists rather than just a few times per year aboard a returning cargo resupply vehicle.
According to smallsat logistics company ÅAC Microtech, a main power distribution board designed for TechEdSat-1 was reused on the TechEdSat-3p mission.{{cite web |url=http://aacmicrotec.com/experience/case/|title=Case|publisher=ÅAC Microtec|access-date=2019-01-31}}
File:Deployment TechEdSat3p.jpg
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TechEdSat-4
{{Infobox spaceflight
| name = TechEdSat-4
| names_list = TES-4
| image =
| image_caption = 290px
| mission_type = Technology demonstration
| operator = NASA Ames Research Center{{·}}San Jose State University{{·}}University of Idaho
| COSPAR_ID = 1998-067FY
| SATCAT = 40455
| mission_duration = {{time interval|13 July 2014, 16:52:14|3 April 2015|show=d}}
| spacecraft_type = CubeSat
| launch_mass = {{cvt|3|kg}}
| dimensions = 10 cm x 10 cm x 30 cm (3U)
| power =
| launch_date = 13 July 2014, 16:52:14 UTC
| launch_rocket = Antares-120
| launch_site = Wallops Island MARS, LP-0A
| launch_contractor = Orbital Sciences Corporation
| deployment_date = 4 March 2015
| decay_date = 3 April 2015
| orbit_reference = Geocentric orbit
| orbit_regime = Low Earth orbit
| orbit_periapsis = 393 km (244 miles)
| orbit_apoapsis = 402 km (250 miles)
| orbit_inclination = 51.64°
| orbit_period = 92.50 minutes
| apsis = gee
}}
TechEdSat-4 was a 3U CubeSat mission developed, integrated, and tested at NASA Ames Research Center in partnership with student interns from San Jose State University (SJSU) in California and the University of Idaho in Moscow, Idaho. The objective of the TechEdSat-4 mission was to demonstrate new technologies including satellite-to-satellite communications and an upgraded Exo-Brake device to demonstrate a passive deorbiting. TechEdSat-4 was launched as a secondary cargo payload on the Cygnus CRS Orb-2 ISS resupply mission. The launch vehicle was the Orbital Sciences Corporation Antares-120, launching from the Mid-Atlantic Regional Spaceport on Wallops Island, Virginia on 13 July 2014.[https://directory.eoportal.org/web/eoportal/satellite-missions/t/techedsat-4 TechEdSat-4 (Technological and Educational Nanosatellite-4)] (access-date 12 September 2014) TechEdSat-4 was deployed from the International Space Station via the Nanoracks CubeSat Deployer on 4 March 2015.{{Cite web|url=https://www.nasa.gov/mission_pages/station/research/experiments/explorer/Investigation.html?#id=1590|title=Experiment Details|website=www.nasa.gov}}{{Cite web|url=https://directory.eoportal.org/web/eoportal/satellite-missions/content/-/article/techedsat-4|title=TechEdSat-4 (Technological and Educational Nanosatellite-4) – Satellite Missions – eoPortal Directory|website=directory.eoportal.org}}
The satellite decayed from orbit on 3 April 2015.{{cite web |url=https://www.n2yo.com/satellite/?s=40455 |title=TECHEDSAT 4 |work=N2YO.com |date=3 April 2015 |access-date=27 May 2022}}
File:ISS-43 Deploying of CubeSats.jpg) Remote Manipulator System (JEMRMS). Deployed satellites included twenty Flock-1b satellites, TechEdSat-4, GEARRSAT, LambdaSat, and MicroMAS.]]
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TechEdSat-5
{{Infobox spaceflight
| name = TechEdSat-5
| names_list = TES-5
| image =
| image_caption =
| image_size = 290px
| mission_type = Technology demonstration
| operator = NASA Ames Research Center{{·}}San Jose State University{{·}}University of Idaho
| COSPAR_ID = 1998-067LB
| SATCAT = 42066
| mission_duration = 144 days
| spacecraft_type = CubeSat
| launch_mass = {{cvt|4|kg}}
| dimensions = 10 cm x 10 cm x 35 cm (3.5U)
| power =
| launch_date = 9 December 2016
| launch_rocket = H-IIB F6
| launch_site = Tanegashima Space Center,
Yoshinobu LC-Y2
| launch_contractor = Mitsubishi Heavy Industries
| deployment_date = 6 March 2017, 18:20:00 UTC
| decay_date = 29 July 2017
| orbit_reference = Geocentric orbit
| orbit_regime = Low Earth orbit
| orbit_periapsis = 397 km (247 miles)
| orbit_apoapsis = 408 km (254 miles)
| orbit_inclination = 51.64°
| orbit_period = 92.61 minutes
| apsis = gee
}}
TechEdSat-5 was a 4 kg, 3.5U CubeSat that was launched on 9 December 2016 aboard the Kounotori 6 (HTV-6) cargo resupply spacecraft, and was deployed from the International Space Station (ISS) at 18:20 UTC on 6 March 2017.{{cite web|url=http://spaceflight101.com/re-entry/re-entry-techedsat-5/|title=Re-Entry: TechEdSat-5|website=spaceflight101.com|date=29 July 2017 |access-date=2018-09-09}} It was the first satellite in the TechEdSat program to include a modulated Exo-Brake that was could adjust the amount of atmospheric drag on the spacecraft, enabling a targeted re-entry.{{cite web|url=https://space.skyrocket.de/doc_sdat/techedsat-5.htm|title=TechEdSat 5 (TES 5)|website=space.skyrocket.de|access-date=2018-09-08}} The TechEdSat-5 Exo-Brake was cross-shaped, made of mylar, and used a combination of mechanical struts and flexible cords. Its surface area was approximately 0.35 square metres. A "Cricket" Wireless Sensor Module (WSM) was included with TechEdSat-5.{{cite news|url=https://www.nasa.gov/ames/image-feature/nasa-parachute-device-may-return-small-spacecraft-from-deep-space-missions|title=NASA Tests Braking Device for Returning Small Spacecraft from Space|last=Minafra|first=Kimberly|date=2017-03-06|publisher=NASA|access-date=2018-09-09}} {{PD-notice}} The satellite reentered the atmosphere on 29 July 2017 after successfully operating for 144 days.{{cite web|url=https://directory.eoportal.org/web/eoportal/satellite-missions/t/techedsat-5|title=TechEdSat5 – eoPortal Directory – Satellite Missions |website=directory.eoportal.org|access-date=2018-09-08}}
File:Sstp_t5p5_with_iss2-1024x678.jpg
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TechEdSat-6
{{Infobox spaceflight
| name = TechEdSat-6
| names_list = TES-6
| image =
| image_caption =
| image_size = 290px
| mission_type = Technology demonstration
| operator = NASA Ames Research Center{{·}}San Jose State University{{·}}University of Idaho
| COSPAR_ID = 1998-067NK
| SATCAT = 43026
| mission_duration = 175 days (achieved)
| spacecraft_type = CubeSat
| launch_mass = {{cvt|3.6|kg}}
| dimensions = 10 cm x 10 cm x 35 cm (3.5U)
| power =
| launch_date = 12 November 2017,
12:19:51 UTC
| launch_rocket = Antares 230
| launch_site = Wallops Island MARS, LP-0A
| launch_contractor = Orbital Sciences Corporation
| deployment_date = 20 November 2017
| decay_date = 14 May 2018
| orbit_reference = Geocentric orbit
| orbit_regime = Low Earth orbit
| orbit_periapsis = {{cvt|397|km}}
| orbit_apoapsis = {{cvt|406|km}}
| orbit_inclination = 51.65°
| orbit_period = 92.59 minutes
| apsis = gee
}}
TechEdSat-6 was a CubeSat 3.5U that was launched at 12:19:51 UTC on 12 November 2017 aboard the Cygnus CRS-8 cargo resupply mission to the International Space Station (ISS).{{cite web|url=https://spaceflight101.com/antares-launches-cygnus-oa8-cargo-spacecraft/|title=Cygnus "S.S. Gene Cernan" En-Route to Space Station after Sunday Morning Commute to Orbit – Spaceflight101 |website=spaceflight101.com|access-date=9 September 2018}}{{cite news|url=https://www.nasa.gov/content/about-techedsat|title=About TechEdSat|last=Phillips|first=Veronica|date=2017-11-10 |publisher=NASA|access-date=8 September 2018}} {{PD-notice}} It was deployed from the Nanoracks CubeSat Deployer on 20 November 2017.{{cite news|url=https://www.nasa.gov/ames/image-feature/nasa-to-test-advanced-space-wireless-sensor-network-and-device-for-returning-small-spacecraft-to-Earth|title=NASA to Test Wireless Network and Device for Returning Smallsats|last=Minafra|first=Kimberly|date=9 November 2017|publisher=NASA|access-date=8 September 2018}} {{PD-notice}} In addition to the primary payload, it contained a CubeSat Identity Tag (CUBIT), a Radio Frequency Identification (RFID) tag developed by DARPA and SRI International to assist in future identification of satellites. It successfully reentered the atmosphere on 14 May 2018.{{cite news|url=https://www.nasa.gov/feature/nasa-ames-astrogram-june-2018|title=Ames Astrogram – June 2018|last=Albaugh|first=Astrid|date=1 June 2018|publisher=NASA|access-date=31 October 2018}} {{PD-notice}}{{Cite web|url=https://www.nasa.gov/mission_pages/station/research/experiments/explorer/Investigation.html?#id=7499|title=Experiment Details|website=www.nasa.gov}}
File:TechEdSat-6.png mission that tested technologies intended to make it easier to return science materials to Earth from space.]]
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TechEdSat-7
{{Infobox spaceflight
| name = TechEdSat-7
| names_list = TES-7
| image =
| image_caption =
| image_size = 290px
| mission_type = Technology demonstration
| operator = NASA Ames Research Center{{·}}San Jose State University
| COSPAR_ID = 2021-002D
| SATCAT = 47312
| mission_duration = 60 days (planned)
{{time interval|17 January 2021, 19:39:00|4 May 2022|show=d|sep=,}} (final)
| spacecraft_type = CubeSat
| launch_mass = {{cvt|3|kg}}
| dimensions = 10 cm x 10 cm x 22 cm (2U)
| power =
| launch_date = 17 January 2021, 19:39:00 UTC
| launch_rocket = LauncherOne
| launch_site = Cosmic Girl (Boeing 747), Mojave Air and Space Port, California
| launch_contractor = Virgin Orbit
| deployment_date = 17 January 2021
| decay_date = 4 May 2022
| orbit_reference = Geocentric orbit
| orbit_regime = Low Earth orbit
| orbit_periapsis = {{cvt|485|km}}
| orbit_apoapsis = {{cvt|513|km}}
| orbit_inclination = 60.7°
| orbit_period = 94.6 minutes
| apsis = gee
}}
TechEdSat-7 was a 2U CubeSat that was intended to test a High Packing Density Exo-Brake. It was launched on the first successful flight of Virgin Orbit's LauncherOne launch vehicle on 17 January 2021 as part of NASA's ELaNa program. It flew with a CubeSat Identity Tag (CUBIT), a Radio Frequency Identification (RFID) tag developed by DARPA and SRI International to assist in future identification of satellites.{{cite web|last=Krebs|first=Gunter|url=https://space.skyrocket.de/doc_sdat/techedsat-7.htm|title=TechEdSat 7 (TES-7)|work=Gunter's Space Page|date=24 August 2021|access-date=12 May 2022}} The satellite decayed from orbit on 4 May 2022.{{cite web |url=https://www.n2yo.com/satellite/?s=47312 |title=OBJECT D |work=N2YO.com |date=4 May 2022 |access-date=12 May 2022}}
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TechEdSat-8
{{Infobox spaceflight
| name = TechEdSat-8
| names_list = TES-8
Technical and Educational Satellite-8
| image =
| image_caption =
| image_size = 290px
| mission_type = Technology demonstration
| operator = NASA Ames Research Center{{·}}San Jose State University{{·}}University of Idaho
| COSPAR_ID = 1998-067PY
| SATCAT = 44032
| mission_duration = {{time interval|5 December 2018, 18:16:00|20 April 2020|show=d}} (achieved)
| spacecraft_type = CubeSat
| launch_mass = {{cvt|6|kg}}
| dimensions = 10 cm x 10 cm x 60 cm (6U)
| power =
| launch_date = 5 December 2018, 18:16:00 UTC
| launch_rocket = Falcon 9 Block 5
| launch_site = Cape Canaveral, SLC-40
| launch_contractor = SpaceX
| deployment_date = 31 January 2019, 16:45 UTC
| entered_service =
| decay_date = 20 April 2020
| orbit_reference = Geocentric orbit
| orbit_regime = Low Earth orbit
| orbit_periapsis = {{cvt|402|km}}
| orbit_apoapsis = {{cvt|409|km}}
| orbit_inclination = 51.64°
| orbit_period = 92.67 minutes
| apsis = gee
}}
TechEdSat-8 (Technical and Educational Satellite-8) was CubeSat 6U. It was built as a conjoined project between San Jose State University (SJSU) and the University of Idaho as a collaborative engineering project, with oversight from the NASA Ames Research Center. It was a technology demonstration mission to further develop and demonstrate the Exo-Brake system through, designed for continued operation in high temperature environments, the full recovery of a payload. It featured a semi-autonomous control system to target the entry face point, as well as capabilities to measure a unique ablation device on the forebody. This technology, known as a "Hot Exo-Brake" could enable more precisely-targeted atmospheric reentries. An ablation device was also flying on the spacecraft.
= History =
TechEdSat-8 was selected in 2017 by the CubeSat Launch Initiative (CSLI) of the NASA to be launched as part of the ELaNa program. TechEdSat-8 was originally planned to launch with the Cygnus NG-10 (17 November 2018) cargo resupply mission to the International Space Station as part of the ELaNa program, but instead was launched aboard the SpaceX CRS-16 ISS cargo resupply mission at 18:16 UTC on 5 December 2018,{{cite web|url=https://blogs.nasa.gov/spacestation/2018/12/04/dragon-launch-slips-one-day-as-new-crew-moves-in/|title=Dragon Launch Slips One Day as New Crew Moves In|publisher=NASA|website=blogs.nasa.gov|date=4 December 2018 |access-date=2018-12-26}} {{PD-notice}} arriving at the International Space Station (ISS) on 8 December 2018.{{cite web|url=https://blogs.nasa.gov/spacestation/2018/12/08/dragon-attached-to-station-returns-to-earth-in-january/|title=Dragon Attached to Station, Returns to Earth in January 2019 – Space Station|website=blogs.nasa.gov|publisher=NASA|access-date=26 December 2018|archive-date=14 December 2018|archive-url=https://web.archive.org/web/20181214122449/https://blogs.nasa.gov/spacestation/2018/12/08/dragon-attached-to-station-returns-to-earth-in-january/|url-status=dead}} {{PD-notice}}{{cite web|url=https://spaceflightnow.com/2018/11/19/space-station-receives-second-of-back-to-back-cargo-deliveries/ |title=Space station receives second of back-to-back cargo deliveries|website=spaceflightnow.com|publisher=Spaceflight Now|access-date=26 November 2018}}
= Deployment =
TechEdSat-8 was deployed into orbit by the Kibō JEM-Small Satellite Orbital Deployer (J-SSOD) at 16:45 UTC on 31 January 2019.{{cite web |url=https://twitter.com/NanoRacks/status/1091016771316912128|title=And, that's a wrap! After an early wake up call this morning, the last #CubeSat deployment from our 15th mission on @Space_Station is now complete! #TechEdSat8 was released at 16:45 UTC. Congratulations to the teams at @NASAAmes and @SJSU – another huge success!pic.twitter.com/ZKqLrnoreQ|last=Nanoracks|date=2019-01-31|website=@NanoRacks|access-date=2019-01-31}}
= Mission =
The satellite established communication with controllers and, as of 20 February 2019, was reportedly performing well in advance of a targeted reentry.{{cite web |url=https://spaceflightnow.com/2019/02/13/cubesat-deployed-from-space-station-to-test-sample-return-technology/|title=CubeSat deployed from space station to test sample return technology|publisher=Spaceflight Now|last=Clark|first=Stephen|access-date=2019-02-20}} The satellite failed shortly after deployment due to a loss of power from its solar panels, and re-entered in the atmosphere of Earth on 20 April 2020.{{cite web|title=Report and Status of the Small Satellite DCS Use Concept Validation Project |url=https://noaasis.noaa.gov/pdf/docs/TWG2019/1330%20Small%20Sat%20Concept.pdf|last=Backus|first=Beau|date=24 April 2019|access-date=10 May 2020}}{{cite web|title=The @techedsat #Techedsat 8 satellite reentered on 20 April 2020. Unfortunately, there's no TIP message to give an accurate reentry time: I hope @NASAAmes @SJSU Marc Murbach et al. (maybe @Ali_AKZAYAKATL ?) will tell us how the controlled entry attempt went.|url=https://twitter.com/planet4589/status/1253425029565435904 |last=McDowell|first=Jonathan|date=2020-04-23|website=@planet4589|access-date=2020-05-10}}
File:TechEdSat-8 Exploded View.jpg
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TechEdSat-10
{{Infobox spaceflight
| name = TechEdSat-10
| names_list = TES-10
| image =
| image_caption =
| image_size = 290px
| mission_type = Technology demonstration
| operator = NASA Ames Research Center{{·}}San Jose State University
| COSPAR_ID = 2020-067RQ
| SATCAT = 45917
| mission_duration = {{time interval|15 February 2020, 20:21:01|15 March 2021, 08:37:00|show=d}} (final)
| spacecraft_type = CubeSat
| launch_mass = {{cvt|6|kg}}
| dimensions = 10 cm x 10 cm x 60 cm (6U)
| power = 150 watt-hour
| launch_date = 15 February 2020, 20:21:01 UTC
| launch_rocket = Antares 230+
| launch_contractor = Northrop Grumman
| deployment_date = 13 July 2020, 16:55:25 UTC
| decay_date = 15 March 2021, 08:37:00 UTC
| orbit_reference = Geocentric orbit
| orbit_regime = Low Earth orbit
| orbit_periapsis = {{cvt|413|km}}
| orbit_apoapsis = {{cvt|419|km}}
| orbit_inclination = 51.60°
| orbit_period = 92.00 minutes
| apsis = gee
}}
TechEdSat-10 (TES-10) was a 6U (1 x 6U) (previously announced as 3U) CubeSat that was selected in 2018 to launch as part of the ELaNa program.{{cite web |last=Krebs|first=Gunter|url=https://space.skyrocket.de/doc_sdat/techedsat-10.htm|title=TechEdSat 10 (TES 10)|publisher=Gunter's Space Page|date=2020-02-20|access-date=13 January 2021}}
= Launch =
On 15 February 2020, TechEdSat-10 was launched to the International Space Station (ISS) aboard the Cygnus NG-13 cargo spacecraft.{{cite web|last=Clark|first=Stephen |url=https://spaceflightnow.com/2020/02/18/cygnus-freighter-delivers-new-british-made-antenna-to-international-space-station/|title=Cygnus freighter delivers new British-made antenna to International Space Station|publisher=Spaceflight Now|date=2020-02-18|access-date=2020-05-17}}
= Deployment =
Deployed on 13 July 2020, TechEdSat-10 tested radio communication devices, precision deorbit technologies for National Oceanic and Atmospheric Administration (NOAA) and others, radiation tolerant electronics, and artificial intelligence hardware for future experiments.{{cite web|last=Hill|first=Denise|url=https://www.nasa.gov/image-feature/cubesat-launch-initiative-deploys-109th-cubesat/ |title=CubeSat Launch Initiative Deploys 109th CubeSat|publisher=NASA|date=2020-07-13|access-date=2020-07-17}} {{PD-notice}}
= Mission =
The mission demonstrated increased storage and power capabilities that could enable future science and exploration using small spacecraft beyond low-Earth orbit. Included on TechEdSat-10 were improvements over previous CubeSat technologies in the areas of communications and radio systems, and new propulsion techniques.{{cite web|url=https://www.nasa.gov/image-feature/ames/techedsat-10-deploys |title=TechEdSat-10 deploys from the International Space Station|publisher=NASA|date=5 August 2020|access-date=14 January 2021}}
As the tenth iteration in the Technology Educational Satellite (TES) series, TechEdSat-10 built upon a history of the program's innovative work with early career researchers, students, and volunteers.
TechEdSat-10 contained 150 watt-hours of power storage, eight radios, nine processors, and a graphics processing unit. Additionally, the small satellite carried four cameras, including a stereoscopic virtual reality camera experiment.
Like several TechEdSat missions before it, this mission demonstrated the exo-brake technology in its largest iteration to date. The exo-brake was designed to deploy an umbrella-like "brake" to increase drag and take a small satellite out of orbit. This mission, the exo-brake could be controlled or modulated by commands from the ground in order to target a re-entry point. In the future, this could enable sample return missions from orbit and future planetary missions.
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TechEdSat-11
{{Infobox spaceflight
| name = TechEdSat-11
| names_list = TES-11
| image =
| image_caption =
| image_size = 290px
| mission_type = Technology demonstration
| operator = NASA Ames Research Center{{·}}San Jose State University
| COSPAR_ID = 2024-125F
| SATCAT = 60208
| mission_duration =
| spacecraft_type = CubeSat
| launch_mass = {{cvt|7|kg}}
| dimensions = (6U)
| power =
| launch_date = 4 July 2024
| launch_rocket = Firefly Alpha
| launch_site = Vandenberg AFB, California
| launch_contractor = Firefly Aerospace
| deployment_date = 4 July 2024, 04:50:01 UTC
| decay_date = UTC
| orbit_reference = Geocentric orbit
| orbit_regime = Low Earth orbit
| orbit_periapsis = {{cvt|490|km}}
| orbit_apoapsis = {{cvt|525|km}}
| orbit_inclination = 97.4°
| orbit_period = 94.8 minutes
| apsis = gee
}}
TechEdSat-11 is a 6U CubeSat. Its goal is to test a set of next-generation communication experiments for CubeSats.
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TechEdSat-13
{{Infobox spaceflight
| name = TechEdSat-13
| names_list = TES-13
| image =
| image_caption =
| image_size = 290px
| mission_type = Technology demonstration
| operator = NASA Ames Research Center{{·}}San Jose State University
| COSPAR_ID = 2022-003B
| SATCAT = 51095
| mission_duration = 252 days (planned)
912 days (actual)
| spacecraft_type = CubeSat
| launch_mass = {{cvt|4|kg}}
| dimensions = 10 cm x 10 cm x 34 cm (3U)
| power =
| launch_date = 13 January 2022
| launch_rocket = LauncherOne # 4
| launch_site = Cosmic Girl (Boeing 747), Mojave Air and Space Port, California
| launch_contractor = Virgin Orbit
| deployment_date = 13 January 2022, 23:47:00 UTC
| decay_date = 13 July 2024, 19:52:00 UTC
| orbit_reference = Geocentric orbit
| orbit_regime = Low Earth orbit
| orbit_periapsis = {{cvt|499|km}}
| orbit_apoapsis = {{cvt|509|km}}
| orbit_inclination = 45.0°
| orbit_period = 92.6 minutes
| apsis = gee
}}
TechEdSat-13 is a 3U CubeSat that is intended to test and validate three different technologies, including an Exo-Brake. Along with other cubesats (PAN-A and B, GEARRS-3, SteamSat-2, STORK-3, ADLER-1) it was launched on the third successful flight of Virgin Orbit's LauncherOne launch vehicle on 13 January 2022 as part of the STP-27VP mission ("Above the Clouds"). TechEdSat-13 uses the Loihi neuromorphic chip, representing an artificial intelligence/machine learning (AI/ML) payload application.
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TechEdSat-15
{{Infobox spaceflight
| name = TechEdSat-15
| names_list = TES-15
| image =
| image_caption =
| image_size = 290px
| mission_type = Technology demonstration
| operator = NASA Ames Research Center{{·}}San Jose State University
| COSPAR_ID = 2022-122?
| SATCAT = 5395?
| mission_duration = {{time interval|1 October 2022, 07:01:00|6 October 2022}} (final)
| spacecraft_type = CubeSat
| launch_mass = {{cvt|4.5|kg}}
| dimensions = 10 cm x 10 cm x 34 cm (3U)
| power =
| launch_date = 1 October 2022, 07:01:00 UTC
| launch_rocket = Firefly Alpha
| launch_site = Vandenberg AFB, California
| launch_contractor = Firefly Aerospace
| deployment_date = 1 October 2022
| decay_date = 6 October 2022
| orbit_reference = Geocentric orbit
| orbit_regime = Low Earth orbit
| orbit_periapsis = {{cvt|215|km}}
| orbit_apoapsis = {{cvt|285|km}}
| orbit_inclination = 137.0°
| orbit_period = 89.6 minutes
| apsis = gee
}}
TechEdSat-15 was a 3U CubeSat. It was launched on 1 October 2022 as a rideshare payload on a Firefly Alpha rocket. Despite it being its first mission reaching Earth orbit, due to a lower-than-intended deployment orbit most of the satellites re-entered before reaching their intended design life.{{cite news |last=Foust |first=Jeff |url=https://spacenews.com/firefly-says-alpha-launch-a-success-despite-payload-reentries/ |title=Firefly says Alpha launch a success despite payload reentries |work=SpaceNews |date=10 October 2022 |access-date=10 October 2022}}
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Future TechEdSats
TechEdSat-9 and TechEdSat-11 are planned to fly at some point in the future.{{cite web|url=https://www.mercurynews.com/2019/01/31/students-at-sjsu-collaborate-with-nasa-to-launch-a-satellite-into-space/# |title=Students at SJSU collaborate with NASA to launch a satellite into space|website=mercurynews.com|date=31 January 2019|access-date=2019-01-31}} TechEdSat-9, like TechEdSat-10, is planned to test radio communication technologies for National Oceanic and Atmospheric Administration (NOAA) and others.
TechEdSat-12 will test technologies for the tracking and identification of small satellites. It will carry a radio-frequency identification (RFID) tag, a radar reflector, and an L-band antenna. It was selected for launch in February 2020 by NASA's CubeSat Launch Initiative, and will be delivered to orbit on a launch contracted through the ELaNa program.{{cite web |url=http://www.nasa.gov/feature/nasa-announces-next-round-of-candidates-for-cubesat-space-missions|title=NASA Announces Next Round of Candidates for CubeSat Space Missions|last=Hill|first=Denise|date=2020-02-21|publisher=NASA|access-date=21 February 2020}} {{PD-notice}}
References
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External links
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Category:Spacecraft launched in 2012
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