Stacked satellite assemblies and related methods

Stacked satellite assemblies and related methods

STACKED SATELLITE ASSEMBLIES AND RELATED METHODS A satellite apparatus is disclosed, including a housing (234, 334) having first (236, 336) and second (238, 338) opposing walls, and a support structure (260, 360) inside the housing (234, 334) spanning the first (236, 336) and second (238, 338) walls...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: ZILZ, Rachel Elizabeth, LANGMACK, Michael John, WOODS, Emily Colleen, HASTINGS, Nicole Marie, ASTON, Richard W
Format: Patent
Sprache:eng
Schlagworte:
AIRCRAFT
AVIATION
COSMONAUTICS
ELECTRIC COMMUNICATION TECHNIQUE
ELECTRICITY
PERFORMING OPERATIONS
SELECTING
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:STACKED SATELLITE ASSEMBLIES AND RELATED METHODS A satellite apparatus is disclosed, including a housing (234, 334) having first (236, 336) and second (238, 338) opposing walls, and a support structure (260, 360) inside the housing (234, 334) spanning the first (236, 336) and second (238, 338) walls. The support structure (260, 360) is structurally connected to the housing (234, 334) only at the first (236, 336) and second (238, 338) walls, and an end portion (262, 362) of the support structure (260, 360) is configured for connection to a launch vehicle (124) by a separation system (106, 410, 412). to 2110 C*4 k" ct C%*4 0000000000000 0 00000 0000000 0 0 a a C.0 (N CD 0 ON 0 (9 CN 0 (2 0 0 (3 C> C%4 0 coo o CN 04 0 CN C14 0 0 0 0 0 0 0 G to 0 (3 C%4 0 CN 0 0 Q C%4 C14 0 0 0 C14 CN 0 0 (D CN 0 0 (3 0 0 00 (D 0 0 V 0 00000 00000 000000000 V C%4 C) V- -1, c:> C> C14 (N C%4