Releasable payload shell for connecting a payload fairing, a pay

Details Releasable payload shell for connecting a payload fairing, a pay Releasable payload shell for connecting a payload fairing, a pay

1998-06-26

2000-07-11

Swiatek, Robert P.

Aeronautics and astronautics

Spacecraft

Spacecraft formation, orbit, or interplanetary path

B64G 100

Patent

active

060860200

ABSTRACT:
A payload section (14) of a rocket, having a payload fairing (16) and a center section (18), which comprises a payload (20) and a payload propulsion unit (22) arranged behind the payload (20) and connected with the payload (20). For preventing, or respectively limiting, a mutual relative movement, the payload fairing (16) and the center section (18) are connected by means of a connection arrangement, which is attached to the payload fairing (16) and also releasably to the center section (18). The connection arrangement is embodied as a preferably flat shell (24), which can consist of two partial shells (24.1, 24.2), which are releasably fastened to each other.

REFERENCES:
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patent: 3706281 (1972-12-01), Hatakeyama
patent: 4699062 (1987-10-01), Lewis et al.
patent: 5322248 (1994-06-01), Ragab
patent: 5331894 (1994-07-01), Wassell et al.
patent: 5372071 (1994-12-01), Richards et al.
patent: 5585596 (1996-12-01), Richards et al.

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