Concepts for more efficient bulkhead designs for launch and space vehicles.
Low profile bulkheads for launch vehicles and spacecraft compartments to obtain structural weight reduction
Engineering topics
Publications and source records attributed to Bernstein, A. I..
Low profile bulkheads for launch vehicles and spacecraft compartments to obtain structural weight reduction
Low profile bulkheads for launch vehicles and spacecraft compartments to obtain structural weight reduction
Mechanical impact attenuation system for Apollo spacecraft provides stable land landing platform, noting deployed heat shields, extended legs, pneumatic bags, etc
Mechanical impact attenuation system for Apollo spacecraft provides stable land landing platform, noting deployed heat shields, extended legs, pneumatic bags, etc
Radial skid and six segment heat shield concepts evaluated for Mechanical Impact System Design for Advanced Spacecraft /MISDAS/
Mechanical impact system for advanced spacecraft application to Apollo spacecraft
Mechanical impact system for earth landing of Apollo command module