Process for recovering a spacecraft first stage

Computer graphics processing and selective visual display system – Display peripheral interface input device – Touch panel

Reexamination Certificate

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Details

C244S158900, C244S159300

Reexamination Certificate

active

07834859

ABSTRACT:
The process comprises the steps of: 1) launching the vehicle from the launch site using the first stage booster rocket engine system; 2) separating the at least one upper stage from the first stage booster; 3) terminating operation of the first booster stage rocket engine system; 4) turning the first stage booster back toward the launch site using the aerodynamic flight control system; 5) operating the first stage booster rocket engine system to boost the first stage booster to an altitude sufficient to allow non-powered flight back to the launch side; and 6) landing the first stage booster at the launch site.

REFERENCES:
patent: 5568901 (1996-10-01), Stiennon
patent: 6158693 (2000-12-01), Mueller et al.
patent: 6450452 (2002-09-01), Spencer et al.
patent: 6454216 (2002-09-01), Kiselev et al.
patent: 6612522 (2003-09-01), Aldrin et al.
patent: 7494089 (2009-02-01), Williams et al.
patent: 2001/0010347 (2001-08-01), Hart et al.
patent: 2003/0192984 (2003-10-01), Smith

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