Cargo/weapons Elevators Parts

(Page 7) End item NSN parts page 7 of 43
Part Number
NSN
NIIN
018-17107 O-ring
001660994
0180-2207 Electrolytic Fixed Capacitor
004129235
019-00004-47 Pipe Bushing
001960930
019-0826-000 Packing Assembly
007888713
019-10A693 Tapered Roller Bearing Cup
001982170
019-1653-150 Electrical Wall Plate
002807921
019-1653-180 Electrical Wall Plate
001881164
01D-10 Hexagon Plain Nut
007646609
01G009701-105 Incandescent Lamp
002704698
01G009701-84 Lug Terminal
008360358
01G009708-6 Lug Terminal
008360358
02-07-0070 Terminal Box
003512222
02-10-3028 Cartridge Fuse
002960361
02-89-5012 Handset Holder
006429879
020-N11 O-ring
005857723
02000-3283 Annular Ball Bearing
002939163
02007-02 Retaining Ring
008206957
021-14374 Hexagon Head Cap Screw
008213869
021-14806 Hexagon Self-locking Nut
002119271
021-16407 O-ring
001661010
Page: 7 ...

Elevators, Cargo/weapons

Picture of Cargo/weapons Elevators

A space elevator is a proposed type of space transportation system.

The concept of a space elevator was first published in 1895 by Konstantin Tsiolkovsky. His proposal was for a free-standing tower reaching from the surface of Earth to the height of geostationary orbit. Like all buildings, Tsiolkovsky's structure would be under compression, supporting its weight from below. Since 1959, most ideas for space elevators have focused on purely tensile structures, with the weight of the system held up from above by centrifugal forces. In the tensile concepts, a space tether reaches from a large mass (the counterweight) beyond geostationary orbit to the ground. This structure is held in tension between Earth and the counterweight like an upside-down plumb bob.

To construct a space elevator on Earth the cable material would need to be both stronger and lighter (have greater specific strength) than any known material. Development of new materials which could meet the demanding specific strength requirement is required for designs to progress beyond discussion stage. Carbon nanotubes (CNTs) have been identified as possibly being able to meet the specific strength requirements for an Earth space elevator.

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