Lme, Inc.

Address

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

Information

DUNS:
# of Employees: 72

Ownership Information

Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N

Award Charts




Award Listing

  1. N/A

    Amount: $974,088.00

    N/A

    SBIRPhase II1999Air Force Department 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 ...

    SBIRPhase I1998Air Force Department 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 ...

    SBIRPhase I1998Air Force Department 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 ...

    SBIRPhase II1995Navy Department of Defense
  5. Optimized Mach Number Immune Parachute Deployment Sequencer

    Amount: $91,704.00

    N/A

    SBIRPhase I1994Navy Department 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 ...

    SBIRPhase I1993Air Force Department 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 ...

    SBIRPhase II1988Navy Department of Defense
  8. GENERIC DESIGN OF AN EMERGENCY RECOVERY AND ESCAPE PATH CLEARANCE SUBSYSTEM FOR ROTARY WING VEHICLES

    Amount: $49,726.00

    N/A

    SBIRPhase I1987Navy Department of Defense

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