Search results
Results from the Health.Zone Content Network
The Antares 200 and 200+ first stages are powered by two RD-181 engines, which provide 440 kilonewtons (100,000 lbf) more thrust than the dual AJ26 engines used on the Antares 100. Orbital adapted the existing core stage to accommodate the increased performance in the 200 Series, allowing Antares to deliver up to 6,500 kg (14,300 lb) to low ...
The Antares has flown two major design iterations, the 100 series and 200 series. Both series have used a Castor 30XL as an upper stage but have differed on the first stage. [15] The 100 series used two Kerolox powered AJ26 engines in the first stage and launched successfully four times. The 100 series was retired following a launch failure in ...
It used to be the first stage engines of the Antares 100 rocket series, although those engines are rebranded the AJ-26 and the newer Antares 200 and Antares 200+ rocket series uses the RD-181 for the first stage engines, which is a modified RD-191, but shares some properties like a single combustion chamber unlike the two combustion chambers ...
Northrop's partnership with Firefly comes months after Russia halted deliveries of Antares' original RD-181 engines in retaliation for sanctions the U.S. levied on Moscow over its Feb. 24 invasion ...
Orbital Sciences, NASA and Aerojet conducted this test of an AJ26 engine in 2010 back when the Antares project was known at Taurus II. The rocket engines are repurposed from Soviet moon missions ...
The company decided to discontinue the Antares 100 series and accelerate the introduction of a new propulsion system. The Antares system has been upgraded with newly built RD-181 first-stage engines to provide greater payload performance and increased reliability. [5]
The company decided to discontinue the Antares 100 series and accelerate the introduction of a new propulsion system. The Antares system is being upgraded with newly built RD-181 first stage engines to provide greater payload performance and increased reliability. [17]
The MA-32 is a two-seat design that was originally developed for European microlight competition flying. The aircraft has a standard empty weight of 321 lb (146 kg). It features a cable-braced hang glider -style high-wing, weight-shift controls, an open cockpit, tricycle landing gear and a single engine in pusher configuration.