Country of origin | Japan |
---|---|
Designer | IHI Aerospace |
Associated LV | HTV, Cygnus |
Status | In production |
Liquid-fuel engine | |
Propellant | N2O4 / Hydrazine |
Cycle | Pressure fed |
Configuration | |
Chamber | 1 |
Performance | |
Thrust, vacuum | 500 N (110 lbf) |
Dimensions | |
Length | 80 cm (31 in) |
Dry weight | 4 kg (8.8 lb) |
The BT-4 is a pressure-fed liquid rocket engine designed and manufactured by IHI Aerospace of Japan. It was originally developed for the LUNAR-A project, but it has been used as a liquid apogee engine in some geostationary communications satellite based on the Lockheed Martin A2100 and GEOStar-2 satellite buses. It has also been used on the HTV and Cygnus automated cargo spacecraft.
During the 1970s, Ishikawajima-Harima Heavy Industries had built under license the Rocketdyne MB-3 for the N-I rocket, for which it had also developed the second stage attitude control system. [1] [2] In the 1980s it also developed the thrusters for ETS-4 ( Kiku-3), the first to be built in Japan. In 2000 it acquired and merged with the aerospace division of Nissan and became IHI Aerospace. [2]
IHI Aerospace started developing the BT-4 for the later cancelled LUNAR-A mission to the moon. While the mission was cancelled, the thruster has seen success as a liquid apogee engine on the Lockheed Martin A2100 and Orbital ATK GEOStar-2 platforms. [3] Two other Orbital ATK products that use the BT-4 due to their leverage of the GEOStar-2 platform are the Cygnus spacecraft and the Antares Bi-propellant Third Stage (BTS). [4] [5] [6] [7] [8] [9]
The use on the A2100 platform has allowed IHI to export the BT-4 even to American military programs such programs as the MUOS and AEHF. [10] [11] [12] [13] [14]
On March 9, 2006, IHI Aerospace announced that the AEHF-2 BT-4 engine had successfully performed its mission, unlike AEHF-1's. [14] [15] [16] On November 29, 2010 IHI Aerospace announced that it had received and order from Lockheed Martin of four BT-4 engines for AEHF-4, MUOS-4, MUOS-5 and Vinasat-2. With this order, it achieved its 100th-unit foreign engine export since it started selling abroad in 1999. [17] [18]
For the HTV project, IHI developed a new version, the HBT-5, which enabled them to replace the American R-4D from the third flight onward. [19] [20]
On October 3, 2013, with the successful berthing of the Cygnus Orb-D1 mission, IHI announced that the propulsion was based on their 500N Delta-Velocity Engines. [21]
In January 2018, a BT-4 kick motor was used on the GovSat-1 geosynchronous commsat flight. [22]
The BT-4 is a family that has been used as liquid apogee engine, orbital maneuvering engine and as a thruster. Known variations:
Country of origin | Japan |
---|---|
Designer | IHI Aerospace |
Associated LV | HTV, Cygnus |
Status | In production |
Liquid-fuel engine | |
Propellant | N2O4 / Hydrazine |
Cycle | Pressure fed |
Configuration | |
Chamber | 1 |
Performance | |
Thrust, vacuum | 500 N (110 lbf) |
Dimensions | |
Length | 80 cm (31 in) |
Dry weight | 4 kg (8.8 lb) |
The BT-4 is a pressure-fed liquid rocket engine designed and manufactured by IHI Aerospace of Japan. It was originally developed for the LUNAR-A project, but it has been used as a liquid apogee engine in some geostationary communications satellite based on the Lockheed Martin A2100 and GEOStar-2 satellite buses. It has also been used on the HTV and Cygnus automated cargo spacecraft.
During the 1970s, Ishikawajima-Harima Heavy Industries had built under license the Rocketdyne MB-3 for the N-I rocket, for which it had also developed the second stage attitude control system. [1] [2] In the 1980s it also developed the thrusters for ETS-4 ( Kiku-3), the first to be built in Japan. In 2000 it acquired and merged with the aerospace division of Nissan and became IHI Aerospace. [2]
IHI Aerospace started developing the BT-4 for the later cancelled LUNAR-A mission to the moon. While the mission was cancelled, the thruster has seen success as a liquid apogee engine on the Lockheed Martin A2100 and Orbital ATK GEOStar-2 platforms. [3] Two other Orbital ATK products that use the BT-4 due to their leverage of the GEOStar-2 platform are the Cygnus spacecraft and the Antares Bi-propellant Third Stage (BTS). [4] [5] [6] [7] [8] [9]
The use on the A2100 platform has allowed IHI to export the BT-4 even to American military programs such programs as the MUOS and AEHF. [10] [11] [12] [13] [14]
On March 9, 2006, IHI Aerospace announced that the AEHF-2 BT-4 engine had successfully performed its mission, unlike AEHF-1's. [14] [15] [16] On November 29, 2010 IHI Aerospace announced that it had received and order from Lockheed Martin of four BT-4 engines for AEHF-4, MUOS-4, MUOS-5 and Vinasat-2. With this order, it achieved its 100th-unit foreign engine export since it started selling abroad in 1999. [17] [18]
For the HTV project, IHI developed a new version, the HBT-5, which enabled them to replace the American R-4D from the third flight onward. [19] [20]
On October 3, 2013, with the successful berthing of the Cygnus Orb-D1 mission, IHI announced that the propulsion was based on their 500N Delta-Velocity Engines. [21]
In January 2018, a BT-4 kick motor was used on the GovSat-1 geosynchronous commsat flight. [22]
The BT-4 is a family that has been used as liquid apogee engine, orbital maneuvering engine and as a thruster. Known variations: