Engineering:GLL-8 (Gll-VK) Igla

From HandWiki

GLL-8 (GLL-VK), nicknamed "Igla" (eng. needle), is a Russian hypersonic flight flying laboratory. It saw its first flight in 2005. It is part of Russia's ongoing ORYOL-2-1 research programme. Under ORYOL-2-1, the Gromov Flight Research Institute in Moscow has developed two possible Igla designs,[1][2] and is leading an SSTO spaceplane effort and a two-stage-to-orbit design conceived to build a "Mir-2" space station.[1][3][4][5]

Purpose

The purpose of this "flying laboratory" is technical data study of hypersonic speeds, which cannot be done with average engines, and other crewed experimental flight-craft. This study includes the following:

  • Aerodynamic properties at hyper sonic speeds
  • Maneuverability at different speeds
  • G-force effects on fuselage at high speeds
  • Scramjet studies[6]

Vehicles associated with the GLL-8

GLL-AP
Vehicle Speed Altitude Length Mass Firing duration Details
GLL-31 Mach 2-9 18–35 km 8 m 3,800 kg 50 s Aircraft dropped, hydrogen-fueled scramjet engine
GLL-8 (GLL-VK) Mach 15 70 km 8 m 2,200 kg 20-50 s Rocket-launched, hydrogen-fueled three-mode scramjet engine
GLL-AP-02 Mach 6 27 km 3 m 550–600 kg Missing data Hydrocarbon-based fueled ramjet prototype for high-altitude test stand tests[2]

References