The use of cryogenic solid hydrogen as a rocket propellant may lead to major advances in rocket propulsion. To use solid hydrogen as a propellant requires a system designed to solidfy, store, and tran ...SBIR Phase I 1993 Air Force Department of Defense
N/ASBIR Phase II 1993 National Aeronautics and Space Administration
N/ASBIR Phase I 1992 National Aeronautics and Space Administration
A CRYOCOOLER IS PROPOSED FOR SPACE-BORNE INFRARED ASTRONOMICAL TELESCOPES WHICH REQUIRE 50 MW OR LESS COOLING AT 1 TO 2 K. IT CONSISTS OF A LINEAR DRIVE THREE STAGE SPLIT-STIRLING CRYOCOOLER WHICH WIL ...SBIR Phase II 1990 National Aeronautics and Space Administration
A MINIATURE TWO STAGE JOULE-THOMSON (J-T) CRYOSTAT IN A DEWAR WITH 0.5 IN. DIA X 0.5 IN. LENGTH IS PROPOSED WHICH CAN COOL TO LESS THAN 80 K IN AN AMBIENT OF 75 DEG C. HIGH EFFICIENCY IN THE VERY SMAL ...SBIR Phase II 1990 Navy Department of Defense
N/ASBIR Phase I 1988 National Aeronautics and Space Administration
N/ASBIR Phase I 1988 Navy Department of Defense
Apd Cryogenics Inc.
| 1833 Vultee St.
Allentown, PA, 18103
|Socially and Economically Disadvantaged:||N|
|Number of Employees:||n/a|