The Orbital Refueling System (ORS); force torque sensor; Plasma Motor/Generator (PMG) proof of function; voice controlled system; infrared intercommunications; superfluid helium on orbit transfer; laser docking sensor; and the Small Expendable Deployment System (SEDS) are summarized.
Flight Demonstration Program and Selection Process
1987
8 pages
Report
No indication
English
The flight demonstration program and selection process
NTRS | 1987
|YAV-8B flight demonstration program
AIAA | 1983
|The NASA Flight Demonstration Program
NTRS | 1985
|Satellite Servicer System Flight Demonstration Program
NTIS | 1989
|