Kounotori 6
Mission type | ISS resupply | ||
---|---|---|---|
Operator | JAXA | ||
Spacecraft properties | |||
Spacecraft type | HTV | ||
Start of mission | |||
Launch date | December 9th 2016 [1] | ||
Rocket | H-IIB 304 | ||
Launch site | Tanegashima Y2 | ||
Contractor | Mitsubishi | ||
Orbital parameters | |||
Reference system | Geocentric | ||
Regime | Low Earth | ||
Inclination | 51.6 degrees | ||
Epoch | Planned | ||
Berthing at ISS | |||
Berthing port | Harmony nadir | ||
Cargo | |||
Mass | 5.9 t | ||
Pressurised | 3.9 t | ||
Unpressurised | 1.9 t | ||
|
Kounotori 6 (こうのとり6号機), also known as HTV-6, will be the sixth flight of the H-II Transfer Vehicle, an unmanned cargo spacecraft launched to resupply the International Space Station.
Originally scheduled for September 2016, the launch was postponed to December 9th due to piping leakage.[1]
Spacecraft
Major changes from previous Kounotori include:[2][3]
- Built-in payloads to demonstrate new technologies: SFINKS and KITE, described below,
- Reduction of primary batteries to 6 from previous 7,
- Reduction of solar cell panels to 48 from previous 49,
- Omission of some of navigation/position lights which were Earth-side when approaching to ISS.
- Strengthened EP (Exposed Pallet) maximum payload to 1.9 t from previous 1.6 t to carry Li-ion batteries.
SFINKS (Solar Cell Film Array Sheet for Next Generation on Kounotori Six) will test thin film solar cells in space.[4]
KITE (Kounotori Integrated Tether Experiment) is an experimental electrodynamic tether (EDT).[5][6] The tether is equipped with a 20 kg end-mass, and will be 700 m long when deployed.[5] A maximum 10 mA current will run through the tether.[5] Kounotori's ISS rendezvous sensor will be utilized to measure how the end-mass moves during the test.[5] The EDT experiment will be conducted following Kounotori 6's departure from the ISS, and is to be held for a week.[5] After the experiment, the tether will be separated before the spacecraft proceeds with the de-orbit maneuvers. The main objective of this experiment is the orbital demonstration of both extending an uncoated bare-tether, and driving electric currents through the EDT.[6] These two technologies will contribute to gaining capabilities to remove space debris.[6]
Cargo
Kounotori 6 carries about 5.9 t of cargo, consisting of 3.9 t in PLC (Pressurised Logistics Carrier) and 1.9 t in ULC (Unpressurised Logistics Carrier).[7]
Cargo in the pressurized compartment includes 30 bags filled with potable water (600 liters),[8][9] food, crew commodities, CDRA Bed (Carbon Dioxide Removal Assembly), TPF (Two-Phase Flow) experiment unit, PS-TEPC (Position-Sensitive Tissue Equivalent Proportional Chamber) radiation measurement instrument, ExHAM (Exposed Experiment Handrail Attachment Mechanism), HDTV-EF2 hi-def and 4K camera, new J-SSOD (JEM Small Satellite Orbital Deployer), and CubeSats (AOBA-Velox III, TuPOD which comprises two TubeSats (Tancredo-1 and OSNSAT), EGG, ITF-2, STARS-C, FREEDOM, WASEDA-SAT3).[10][11][7]
Cargo in the unpressurized compartment consists of six Lithium-ion batteries and their associated adapter plates to replace existing nickel-hydrogen batteries of the ISS. Since each of the new Li-ion battery has a capability equivalent to two of the current Ni-H batteries, the six new batteries will replace twelve old batteries, out of the 48 existing batteries of the ISS.[8]
On departure from the ISS, Kounotori 6 will carry 9 out of the 12 replaced old batteries which will be disposed by destructive reentry into Earth's atmosphere. The 3 remaining old batteries will stay on the ISS.[9]
Operation
Launch
On 26 July 2016, the launch was scheduled for 30 September 2016,[12] but on 10 August 2016, postponement was announced due to the leak from piping.[13]
References
- 1 2 "JAXA Press Release". JAXA. 7 October 2016. Retrieved 7 October 2016.
- ↑ JAXA (1 July 2016). 宇宙ステーション補給機「こうのとり」6号機(HTV6)の概要(その2) (PDF). 宇宙開発利用部会 調査・安全小委員会(第19回) 配付資料 (in Japanese). Retrieved 10 July 2016.
- ↑ JAXA (1 July 2016). 宇宙ステーション補給機「こうのとり」6号機(HTV6)の接近・係留・離脱フェーズに係る安全検証結果について (PDF). 宇宙開発利用部会 調査・安全小委員会(第19回) 配付資料 (in Japanese). Retrieved 10 July 2016.
- ↑ "研究成果(より詳細な研究内容)" (in Japanese). JAXA Research and Development Directorate. Retrieved 2016-07-07.
- 1 2 3 4 5 "HTV搭載導電性テザー実証実験の検討状況について" (PDF) (in Japanese). JAXA. 2013-09-04. Retrieved 26 December 2014.
- 1 2 3 "JAXA、宇宙ゴミ除去技術の確立に向け「こうのとり」利用" (in Japanese). Response staff. 2013-09-09. Retrieved 21 March 2015.
- 1 2 宇宙ステーション補給機「こうのとり」6号機(HTV6)【ミッションプレスキット】 (PDF) (in Japanese). JAXA. 24 November 2016. Retrieved 3 December 2016.
- 1 2 「こうのとり」6号機へのISSバッテリ搭載作業、水充填装置のプレス公開 (in Japanese). JAXA. June 3, 2016. Retrieved June 3, 2016.
- 1 2 国際宇宙ステーション用バッテリ・飲料水充填装置説明会 (in Japanese). NVS. June 1, 2016. Retrieved June 3, 2016.
- ↑ 「こうのとり」6号機に搭載する超小型衛星7基を公開しました (in Japanese). JAXA. November 7, 2016. Retrieved November 8, 2016.
- ↑ "TuPOD almost ready for launch". Group of Aerodynamics for the Use of Space Systems. July 27, 2016. Retrieved November 8, 2016.
- ↑ "Launch of the H-II Transfer Vehicle "KOUNOTORI6" (HTV6) aboard the H-IIB Launch Vehicle No. 6". JAXA. 26 July 2016. Retrieved 10 August 2016.
- ↑ "Launch Postponement of H-IIB Launch Vehicle No. 6 with H-II Transfer Vehicle "KOUNOTORI6" (HTV6) Onboard". JAXA. 10 August 2016. Retrieved 10 August 2016.
External links
- JAXA HTV page
- 宇宙開発最前線! Vol.6 (PDF) (Japanese)
Images
- Kounotori 6 - JAXA Digital Archives
- HTV-6 & KITE
- HTV-6 & KITE