MICROCOSM  Sprite

 
 

Microcosm Inc. * Scorpius Space Launch Comp.
 

Established in 1984, Microcosm Inc. is a small business, specializing in reducing space mission cost. Our experience covers commercial, military, and scientific missions from small, low-cost programs to multi-billion dollar, multi-satellite constellations and a family of launch vehicles.

The Scorpius rocket family is a new generation of expendable launch vehicles intended to reduce the cost of launch to orbit by a factor of 5 to 10. The Scorpius program is a total "clean-sheet" development using new technologies for pressure-fed, LOX/Jet-A propellants, all new low cost ablative engines, and GPS/INS guidance/control. Funding for the ongoing Scorpius program has been provided primarily by the Air Force, Ballistic Missile Defense Organization (BMDO), NASA, and Microcosm internal R&D.

Scorpius SR-M: Sounding rocket
Configuration: 38.4 ft. long, 42 in. diameter , 4 rear fins, gross weight 13,700 lb.
Engine: Single Microcosm Scorpius 20,000 lbf. (vacuum) thrust engine, ablatively-cooled. Pressure-fed using High Performance Pressurization System (HPPS). Propellants: Kerosene (Jet-A)/LOX in all-composite tanks with 42 in. diameter.
Variant SR-M2 with Sprite upper stage for tests.

Scorpius Sprite: Mini-Lift Launch Vehicle
SR-M with upper stage and six 45-inch diameter pods around a central core. Uses much of the suborbital technology and approach. Performance: 810 lbs. to Low Earth Orbit.
Configuration: 54,2 ft. long, booster pods & core sustainer pod with 45 in. diameter,  6 rear fins. Overall diameter 11.2 ft.  Dry weight: 12,300 lb. Wet weight:  83,000 lb.
Engines: Six  20K lb engines, one 20K lb engine, one 2.3K lb engine. Single Microcosm Scorpius 20K lb  (vacuum) thrust engine, ablatively-cooled. Pressure-fed using High Performance Pressurization System (HPPS). Propellants: Kerosene (Jet-A)/LOX in all-composite tanks with 42 in. diameter.
Variant SR-2 without Sprite upper stage.

Microcosm successfully completed the first test flight of the Scorpius™ SR-XM-1 dual engine suborbital rocket at the White Sands Missile Range, New Mexico on March 9, 2001. The SR-XM-1 flight used the ultra-low-cost Scorpius 5,000 lb. thrust engines, avionics, and composite fuel tank. The vehicle is the first of a new liquid booster family and is the successor of the smaller SR-S launched in January, 1999.
The next steps in the Scorpius program will be the continued development and testing of low-cost Scorpius components and the launch of the SR-XM-2 Vehicle that will use the larger 20,000 lb. thrust engine currently in development. This new engine is a derivative of the flight-proven engines. Engine testing will be done at the Energetic Materials Research Test Center (EMRTC) Rocket Test Site in Socorro, NM. Development of the SR-XM and larger vehicles is underway at the Microcosm facilities in El Segundo, CA.


Test flight SR-XM-1 in 2001


The SR-M, comprised by a single engine, capable of 20,000 pounds of thrust, is anticipated to also be launched from White Sands Missile Range in early 2007. The SR-M will be essentially a single pod of a multi-pod design (a core with six surrounding pods) called Sprite, which will be capable of placing small satellites in orbit.