Lme, Inc.

Basic Information

P.O. Box 6637
201 Defense Highway, Suite 201
Annapolis, MD, 21401

Company Profile

n/a

Additional Details

Field Value
DUNS: n/a
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 72


  1. N/A

    Amount: $974,088.00

    N/A

    SBIR Phase II 1999 Air ForceDepartment of DefenseDepartment of Defense
  2. High Energy Absorbing Troop Seat Study

    Amount: $98,282.00

    During a crash of a troop-carrying fixed wing aircraft or helicopter the troop seats have been designed to withstand the specification force levels without regard for any protection of the seat occupa ...

    SBIR Phase I 1998 Air ForceDepartment of DefenseDepartment of Defense
  3. Study of the Spinal Preloading Piston for the CKU-5/A Rocket Catapult

    Amount: $99,257.00

    Small, light weight, female pilots have been introduced into the AF and Navy pilot population in recent years. The increased spinal loading of light weight ejectees during the catapult stroke, with i ...

    SBIR Phase I 1998 Air ForceDepartment of DefenseDepartment of Defense
  4. Optimized Mach Number Immune Parachute Deployment Sequencer

    Amount: $507,614.00

    Shock waves which form forward of an occupied ejection seat in a supersonic airstream can produce static and total pressure values which indicate safe altitude/airspeed conditions suitable for recover ...

    SBIR Phase II 1995 NavyDepartment of DefenseDepartment of Defense
  5. Optimized Mach Number Immune Parachute Deployment Sequencer

    Amount: $91,704.00

    N/A

    SBIR Phase I 1994 NavyDepartment of DefenseDepartment of Defense
  6. Spinal Pre-Loading Catapult for Escape Systems for ALCF

    Amount: $72,859.00

    Some of the advantages of the SPINAL PRE-LOADING CATAPULT are given and the theoretical basis for its design is provided. The results of a study indicate improved performance levels that can be expect ...

    SBIR Phase I 1993 Air ForceDepartment of DefenseDepartment of Defense
  7. GENERIC DESIGN OF AN EMERGENCY RECOVERY AND ESCAPE PATH CLEARANCE SUBSYSTEM FOR ROTARY WING VEHICLES

    Amount: $381,000.00

    INFLIGHT RECOVERY OR ESCAPE FROM A DISABLE HELICOPTER REQUIRES THAT THE ROTOR BLADES NOT INTERFERE WITH THE ORDERLY OPERATION OF THE EMERGENCY SYSTEM THAT WILL RETURN THE OCCUPANTS SAFELY TO EARTH. TH ...

    SBIR Phase II 1988 NavyDepartment of DefenseDepartment of Defense
  8. GENERIC DESIGN OF AN EMERGENCY RECOVERY AND ESCAPE PATH CLEARANCE SUBSYSTEM FOR ROTARY WING VEHICLES

    Amount: $49,726.00

    N/A

    SBIR Phase I 1987 NavyDepartment of DefenseDepartment of Defense

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