Английская Википедия:Black Brant (rocket)
The Black Brant is a family of Canadian-designed sounding rockets originally built by Bristol Aerospace, since absorbed by Magellan Aerospace in Winnipeg, Manitoba. Over 800 Black Brants of various versions have been launched since they were first produced in 1961, and the type remains one of the most popular sounding rockets.[1] They have been repeatedly used by the Canadian Space Agency and NASA.
History
Black Brant was the result of research at Canadian Armament Research and Development Establishment (CARDE) during the 1950s into the nature of the upper part of the atmosphere as part of ongoing research into anti-ballistic missile systems and very-long-range communication. In 1957 CARDE contracted Bristol to produce a simple rocket fuselage, called the Propulsion Test Vehicle, for studies into high-power solid fuels. The resulting design, by Albert Fia, was quite heavy, as it was designed to be able to accommodate a wide variety of engine burning times, propellant loadings and launch angles in keeping with its role as a test vehicle for ABM systems development. The first test flight took place only two years later from the Churchill Rocket Research Range in September 1959.[2]
CARDE's attention later turned to long-distance communications and they found the Propulsion Test Vehicle system useful as a sounding rocket. To better suit this role, Bristol modified the design to be lighter and more tailored to the sounding rocket role. This became the Black Brant. CARDE launched a number of Black Brant rockets over the next few years, both the original Black Brant I design which could place a Шаблон:Convert payload to Шаблон:Convert altitude, as well as the larger Шаблон:Nowrap which first flew in October 1960, and the smaller but higher-altitude Шаблон:Nowrap.
The rocket's design emphasized reliability over payload and range.[3] In July 1963 the much larger Шаблон:Nowrap first flew, which was also used as a booster stage for the Шаблон:Nowrap to make the Шаблон:Nowrap. The IV first flew in 1964, but failed, as did the next test launch. Aside from these two launches, which were corrected for, the Шаблон:Nowrap has never had another failure, making it one of the most reliable rockets in history. Since then it has undergone continual evolution, and the current versions are the XI and XII, consisting of Шаблон:Nowrap used as an upper stage, with Talos and Terrier boosters as lower stages. They have reached altitudes of more than Шаблон:Convert, which is above the ionosphere and well above the orbits of the Space Shuttle and the International Space Station.
The propellant designs developed by CARDE in the Шаблон:Nowrap program were the highest performing solid fuels of their day. Bristol then placed this propellant in a new Шаблон:Convert rocket to form the CRV7, the first rocket capable of penetrating standard Warsaw Pact aircraft hangars. The CRV7 has since gone on to become the de facto standard rocket for most Western-aligned militaries.
In 1976, Australia and Canada through the National Research Council Canada (NRCC) agreed[4] to launch a rocket from Woomera Test Range. The Шаблон:Nowrap rocket was launched there on 9 November for experiments in the ionosphere.[5] Later, NASA would launch a number of Шаблон:Nowrap.
At present, due to its 98% success rate, it remains one of the most popular sounding rockets ever built. The rockets have been used repeatedly by the Canadian Space Agency and NASA. There is a 1:1 scale model of the Шаблон:Nowrap rocket in front of the head office of the Canadian Space Agency in Saint-Hubert, east of Montréal. A full-scale Шаблон:Nowrap is on display in the Science Gallery of The Manitoba Museum in Winnipeg, Manitoba, Canada.
In 1995, a Black Brant XII four-stage sounding rocket from the Andøya Rocket Range off the northwestern coast of Norway caused the Norwegian rocket incident, also known as the Black Brant scare. The trajectory resembled that of a U.S. Navy submarine-launched Trident missile. Russian nuclear forces were put on high alert as a result, fearing a high-altitude nuclear attack that could blind Russian radar, and Russia's "nuclear briefcase", the Cheget, was brought to Russian President Boris Yeltsin, who then had to decide whether to launch a retaliatory nuclear strike against the United States. It is the first and thus far only known incident where any nuclear-weapons state had its nuclear briefcase activated and prepared for launching an attack.
On September 19, 2009, a Black Brant XII that was launched to study clouds caused numerous calls from the northeastern U.S. reporting "strange lights in the sky". NASA reported that the light came from an artificial noctilucent cloud formed by the exhaust particles of the rocket's fourth stage at an altitude of about Шаблон:Convert.
Versions
the following is enumerated by roman numerals
Black Brant I
- Black Brant I[6]
- Payload: Шаблон:Convert
- Maximum flight height: Шаблон:Convert
- Launch thrust: Шаблон:Convert
- Launch mass: Шаблон:Convert
- Diameter: Шаблон:Convert
- Length: Шаблон:Convert
Black Brant II
- Black Brant II,[7] Black Brant IIB[8]
- Payload: Шаблон:Convert (Black Brant II)
- Maximum flight height: Шаблон:Convert
- Thrust: Шаблон:Convert
- Mass at launch: Шаблон:Convert
- Diameter: Шаблон:Convert
- Length: Шаблон:Convert
The II was the first rocket for scientific use and was ready in 1960.[9]
Black Brant III
- Black Brant III,[10] Black Brant IIIA, Black Brant IIIB[11]
- Payload: Шаблон:Convert (Black Brant III)
- Maximum flight height: Шаблон:Convert
- Thrust: Шаблон:Convert
- Mass at launch: Шаблон:Convert
- Diameter: Шаблон:Convert
- Length: Шаблон:Convert
Black Brant IV
- Black Brant IV is a two-stage rocket consisting of Black Brant VA first stage with either a Black Brant IIIA or IIIB second stage,[12] Black Brant IVA,[13] Black Brant IVB[14]
- Payload: Шаблон:Convert (Black Brant IV)
- Maximum flight height: Шаблон:Convert
- Thrust: Шаблон:Convert
- Mass at launch: Шаблон:Convert
- Diameter: Шаблон:Convert
- Length: Шаблон:Convert
Black Brant V
- Black Brant V,[15] Black Brant VA,[16] Black Brant VB,[17] Black Brant VC[18]
- Payload: Шаблон:Convert (Black Brant V)
- Maximum flight height: Шаблон:Convert
- Thrust: Шаблон:Convert
- Mass at launch: Шаблон:Convert
- Diameter: Шаблон:Convert
- Length: Шаблон:Convert
Black Brant VI
- Black Brant VI[19]
- Maximum flight height: Шаблон:Convert
- Thrust: Шаблон:Convert
- Mass at launch: Шаблон:Convert
- Diameter: Шаблон:Convert
- Length: Шаблон:Convert
Black Brant VII
- Black Brant VII[20]
- Maximum flight height: Шаблон:Convert
- Thrust: Шаблон:Convert
- Mass at launch: Шаблон:Convert
- Diameter: Шаблон:Convert
- Length: Шаблон:Convert
Black Brant VIII
- Black Brant VIII (a.k.a. Nike Black Brant) is a two-stage rocket with a Nike M5-E1 booster first stage and either a Black Brant VB or VC second stage,[21][22] Black Brant VIIIB,[23] Black Brant VIIIC[24]
- Maximum flight height: Шаблон:Convert (Black Brant VIII)
- Thrust: Шаблон:Convert
- Mass at launch: Шаблон:Convert
- Diameter: Шаблон:Convert
- Length: Шаблон:Convert
Black Brant IX
- Status: Active
- Black Brant IX (a.k.a. Terrier Black Brant) is a two-stage rocket with a Terrier Mk 70 booster first stage and a Black Brant VB second stage,[25][26] Black Brant IXB,[27] Black Brant IXBM1,[28] Black Brant IXCM1,[29] Terrier Black Brant XI Mod 2[30][31]
- Maximum flight height: Шаблон:Convert
- Mass at launch: Шаблон:Convert (Black Brant IX)
- Diameter: Шаблон:Convert
- Length: Шаблон:Convert
- First launch: 1982-03-16
- Last launch: 2023-10-30 05:45 UTC (INFUSE)
- Total launches: 321
- Successful launches: 315
Black Brant X
- Black Brant X (a.k.a. Terrier Black Brant Nihka) is a three-stage rocket with a Terrier Mk 70 booster first stage, a Black Brant VB or VC second stage and a Nihka third,[32][33] Black Brant XB,[34] Black Brant XCM1[35]
- Payload: Шаблон:Convert (Black Brant X)
- Maximum flight height: Шаблон:Convert
- Thrust: Шаблон:Convert
- Mass at launch: Шаблон:Convert
- Diameter: Шаблон:Convert
- Length: Шаблон:Convert
Black Brant XI
- Black Brant XI (a.k.a. Talos Taurus Black Brant) is a three-stage rocket with a Talos booster first stage, Taurus booster second stage, and a Black Brant V third stage,[36][37][38] Black Brant XIA
- Payload: Шаблон:Convert to Шаблон:Convert altitude, or Шаблон:Convert to Шаблон:Convert altitude (Black Brant XI)
- Maximum flight height: Шаблон:Convert
- Thrust:
- Mass at launch: Шаблон:Convert
- Diameter: Шаблон:Convert
- Length: Шаблон:Convert
Black Brant XII
- Black Brant XII (a.k.a. Talos Terrier Black Brant Nihka) is a four-stage rocket with a Mk 11 Mod 5 Talos booster first stage, Terrier booster second stage (pre 2013 Taurus booster motors were used), Black Brant V third stage and Nihka fourth stage,[39][40] Black Brant XIIA[41]
- Payload: manufacturer rated from Шаблон:Convert (Black Brant XII)
- Maximum flight height: Approximately Шаблон:Convert, dependent on payload
- Thrust: 116,001 lbf first stage Talos booster[42]
- Mass at launch: Approximately Шаблон:Convert, dependent on payload
- Diameter:
- Length: Шаблон:Convert
- First launch: 30 September 1988 (BEARS)
- Last launch: 9 November 2023 (Beam-PIE)
- Total launches: 35 (28 Black Brant XII, 7 Black Brant XII-A)
- Successful launches: 33 (26 Black Brant XII, 7 Black Brant XII-A)
See also
References
Further reading
- Corliss, William R., NASA Scientific and Technical Information Office (1971), NASA Sounding Rockets, 1958-1968 A Historical Summary, NASA SP-4401. Washington D.C.
External links
- Overview on manufacturer's website (click on Black Brant Rocket), archived version with more details
- Black Brant entry in Encyclopedia Astronautica
- NASA Sounding Rocket User's Handbook
Шаблон:Rocket families Шаблон:Canadian Space Agency
- ↑ Шаблон:Cite web
- ↑ Шаблон:Cite web
- ↑ Шаблон:Cite magazine
- ↑ "Exchange of Notes constituting an Agreement between the Government of Australia and the Government of Canada relating to the Launching of a Canadian Scientific Rocket from Woomera ATS 22 of 1976 " Шаблон:Webarchive. Australasian Legal Information Institute, Australian Treaties Library. Retrieved on 15 April 2017.
- ↑ Шаблон:Cite web
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