Altair (rocket stage)
Solid-fuel rocket
From Wikipedia, the free encyclopedia
The Altair was a solid-fuel rocket with a filament-wound fibre-reinforced epoxy resin casing, initially developed for use as the third stage of Vanguard rockets in 1959.[1] It was manufactured by Allegany Ballistics Laboratory (ABL) as the X-248. It was also sometimes called the Burner 1.
Altair
The X-248 was one of two third-stage designs used during Project Vanguard. Early launches used a stage developed by the Grand Central Rocket Company, but the last used the X-248 which enabled the Vanguard to launch more massive payload.
The X-248 was used as the second stage of some early Thor flights. These vehicles were designated "Thor-LV2D Burner-1".[2][3]
Altairs were used as the third stage of early Delta rockets.[4]
The fourth stage of the Scout-X rocket used the "Altair-1A" stage, powered by a X-248A engine.[5][6]
This initial variant could produce 13.7 kN (3,070 lbf) of thrust, and had a diameter of 43.18 cm (17.00 in).[7]
Altair 2
The Altair 2 (X-258) Thiokol (Star 25, TE-M-184-3) solid rocket engine first flew in 1963 and was the kick stage motor for Delta D, Scout A, Scout X-4, and Atlas-D OV1 as part of the Orbiting Vehicle[8] satellites.[9] It was retired in 1973.[10]
Altair 3
The Altair 3 (FW-4S) solid rocket engine first flew in 1968 and was used on the Atlas-E/F OV1 as part of the OV1 upper stage.[11] It was also used as the second stage of the ASM-135 ASAT anti-satellite missile.[12] It was proposed as the fourth stage for Advanced Scout.[13] The FW-4S motor is similar to Thiokol Star 20 (TE-M-640), and both are designated by NASA as Altair IIIA.[14]
