Terrier Oriole

Last updated
  1. "Jonathan's Space Report Issue 742". 2017-11-25.
  2. "Oriole". Propulsion Products Catalog (PDF). Northrop Grumman. p. 124.
  3. Dunbar, Brian (March 3, 2012). Wilson, Jim (ed.). "NASA's Terrier Oriole Rocket". NASA/GSFC. Archived from the original on April 29, 2023. Retrieved March 16, 2012.
  4. 1 2 3 4 "Terrier Oriole information brochure" (PDF). NASA. Archived (PDF) from the original on 3 December 2024.
  5. Krebs, Gunter Dirk. "Terrier Oriole (Oriole-2)". Gunter's Space Page. Retrieved 2024-06-11.
  6. 1 2 Naval Surface Warfare Center, Port Hueneme Division Public Affairs (April–June 2011). "Ballistic Missile Tracking Exercise Using ARAV-B". CHIPS. Archived from the original on 25 February 2021.
  7. Terrier Terrier combinations, Gunter's space Page, updated to 03.03.2021, accessed 2022-11-23
  8. Japanese destroyers intercept ballistic missiles in tests with US Navy, Mike Yeo, DefenseNews.com, 2022-11-23
  9. "Le vol d'essai du planeur hypersonique VMAX était le fruit d'une collaboration franco-américaine". 12 December 2023.
Terrier Oriole
Terrier Oriole.jpg
Terrier Oriole at launch
FunctionSounding rocket
ManufacturerAstrotech Space Operations
Country of originUnited States
Size
Height8.2 metres (324 in)
Diameter0.56 metres (22 in)
Stages2
Capacity
Payload to 340 kilometres (210 mi)
Mass360 kilograms (800 lb)
Associated rockets
FamilyTerrier
Launch history
StatusOperational
Launch sites Wallops Island, Barking Sands, South Uist [1]
Total launches12 minimum
First flightJuly 7, 2000
First stage – Terrier Mk 12
Height3.9 metres (155 in)
Diameter0.46 metres (18 in)
Gross mass1,001 kilograms (2,207 lb)
Powered by1
Maximum thrust258 kilonewtons (58,000 lbf)
Propellantsolid