Terrier Oriole
{{Infobox rocket
|image = Terrier Oriole.jpg
|caption = Terrier Oriole at launch
|name = Terrier Oriole
|function = Sounding rocket
|manufacturer = Astrotech Space Operations
|country-origin = United States
|height = {{convert|324|in|m|disp=flip}}
|diameter = {{convert|22|in|m|disp=flip}}
|mass =
|stages = 2
|capacities =
{{Infobox rocket/Payload
|location = {{convert|340|km|mi}}
|kilos = {{convert|800|lb|kg|disp=flip}}
}}
|family = Terrier
|derivatives =
|comparable =
|status = Operational
|sites = Wallops Island, Barking Sands, South Uist{{Cite web|url=http://planet4589.org/space/jsr/back/news.742|title=Jonathan's Space Report Issue 742|date=2017-11-25}}
|launches = 12 minimum
|success =
|fail =
|partial =
|other_outcome =
|first = July 7, 2000
|last =
|only =
|payloads =
|stagedata =
{{Infobox rocket/Stage
|type = stage
|stageno = First
|name = Terrier Mk 12
|length = {{convert|155|in|m|disp=flip}}
|diameter = {{convert|18|in|m|disp=flip}}
|empty =
|gross = {{convert|2207|lb|kg|disp=flip}}
|engines = 1
|thrust = {{convert|258|kN|lbf}}
|total =
|SI =
|burntime =
|fuel = solid
}}
{{Infobox rocket/Stage
|type = stage
|stageno = Second
|length = {{convert|155|in|m|disp=flip}}
|diameter = {{convert|22|in|m|disp=flip}}
|empty = {{convert|436|lb|kg|disp=flip}}
|gross = {{convert|2,588|lb|kg|disp=flip}}
|propmass = {{convert|2,152|lb|kg|disp=flip}}
|engines = 1
|thrust = {{convert|29,570|lbf|kN|disp=flip}} (vacuum)
|total =
|SI = 288.5 s (vacuum)
|burntime = 30 seconds
|fuel = QDL/SAA-144 (HTPB-based APCP)
}}
}}
Terrier Oriole is an unguided two-stage rocket system which is primarily used by the Goddard Space Flight Center out of the Wallops Flight Facility as a sounding rocket. The system uses a Terrier first-stage booster attached to an Oriole second-stage rocket.{{Cite web |last=Dunbar |first=Brian |date=March 3, 2012 |editor-last=Wilson |editor-first=Jim |title=NASA's Terrier Oriole Rocket |url=http://www.nasa.gov/mission_pages/sunearth/missions/terrier-improvedOriole.html |archive-url=https://web.archive.org/web/20230429164459/https://www.nasa.gov/mission_pages/sunearth/missions/terrier-improvedOriole.html |archive-date=April 29, 2023 |access-date=March 16, 2012 |publisher=NASA/GSFC}} The system can carry payloads between {{Convert|800|and|1500|lbs}} up to an altitude of {{Convert|320|km}}.{{Cite web |title=Terrier Oriole information brochure |url=http://sites.wff.nasa.gov/code810/vehicles/Terrier_Oriole.pdf |url-status=live |archive-url=https://web.archive.org/web/20241203201854/https://sites.wff.nasa.gov/code810/vehicles/Terrier_Oriole.pdf |archive-date=3 December 2024 |publisher=NASA}} It is also used to test ballistic missile defense systems, under the name ARAV-B.
Technical details
The Terrier motor is {{Convert|18|in}} in diameter and {{Convert|155|in}} long, and it normally uses two "spin motors", both to reduce dispersion and to serve as drag plates. It uses four equally spaced fins which are {{Convert|4.8|ft2}} and canted in such a way as to provide two revolutions per second at Terrier burnout. The weight of the Terrier booster system is {{Convert|2207|lbs}}.
The Oriole stage is {{Convert|22|in}} in diameter and {{Convert|155|in}} long. It is powered by GEM-22 Graphite-Epoxy Motor.{{Cite web |last=Krebs |first=Gunter Dirk |title=Terrier Oriole (Oriole-2) |url=https://space.skyrocket.de/doc_lau_det/terrier_oriole.htm |access-date=2024-06-11 |website=Gunter's Space Page}} There is a {{Convert|14|in|mm|adj=on}} interstage adapter between the Terrier and Oriole systems, which allows for drag separation following Terrier burnout. The Oriole stage uses four fins in a cruciform configuration, which are canted in order to provide a spin rate of four revolutions per second upon Oriole burnout.
Standard hardware includes a nose cone and capacitive discharge ignition system. Separation systems are available for use in order to separate the payload from the motor during ascent. An ogive nose cone is also available to users, when required.
Terrier-Oriole is used to test ballistic missile defense systems, under the name Aegis Readiness Assessment Vehicle-B (ARAV-B).{{Cite news |last=Naval Surface Warfare Center, Port Hueneme Division Public Affairs |date=April–June 2011 |title=Ballistic Missile Tracking Exercise Using ARAV-B |url=https://www.doncio.navy.mil/CHIPS/ArticleDetails.aspx?id=2294 |archive-url=https://web.archive.org/web/20210225065856/https://www.doncio.navy.mil/CHIPS/ArticleDetails.aspx?id=2294 |archive-date=25 February 2021 |url-status=live |work=CHIPS}} It is much cheaper than other ballistic missile targets.
=T4-E=
This T-T-O stack uses two Terrier Mk.70 (TX-664) plus the final Oriole GEM-22 as a medium range ballistic missile (MRBM) target.[https://space.skyrocket.de/doc_lau/terrier_terrier.htm Terrier Terrier combinations], Gunter's space Page, updated to 03.03.2021, accessed 2022-11-23
In mid-November 2022, the T4-E stack was used for two live-fire events when Japanese Navy ships {{JS|Maya}} and {{JS|Haguro}} used RIM-161 SM-3 Block IIA missiles to engage T4-E targets in conjunction with the US Navy at the Pacific Missile Range Facility, Kauai Island, Hawaii.[https://www.defensenews.com/battlefield-tech/2022/11/22/japanese-destroyers-intercept-ballistic-missiles-in-tests-with-us-navy/ Japanese destroyers intercept ballistic missiles in tests with US Navy], Mike Yeo, DefenseNews.com, 2022-11-23
= Terrier-Oriole-Oriole =
A 3-stage rocket (a Terrier booster and two Oriole stages) is used for the test of the VMAX hypersonic glider of the French Ministry of Defense from the Biscarosse test site DGA Essais de missiles in Landes on June 26, 2023.{{Cite web|url=https://meta-defense.fr/2023/12/12/planeur-hypersonique-vmax-us-navy/|title =Le vol d’essai du planeur hypersonique VMAX était le fruit d’une collaboration franco-américaine. | date=12 December 2023 }}
See also
References
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