Space Systems/loral, Inc. v. Lockheed Martin Corporation

271 F.3d 1076, 60 U.S.P.Q. 2d (BNA) 1861, 2001 U.S. App. LEXIS 24360, 2001 WL 1403311
CourtCourt of Appeals for the Federal Circuit
DecidedNovember 13, 2001
Docket00-1269
StatusPublished
Cited by15 cases

This text of 271 F.3d 1076 (Space Systems/loral, Inc. v. Lockheed Martin Corporation) is published on Counsel Stack Legal Research, covering Court of Appeals for the Federal Circuit primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Space Systems/loral, Inc. v. Lockheed Martin Corporation, 271 F.3d 1076, 60 U.S.P.Q. 2d (BNA) 1861, 2001 U.S. App. LEXIS 24360, 2001 WL 1403311 (Fed. Cir. 2001).

Opinion

PAULINE NEWMAN, Circuit Judge.

Space Systems/Loral, Inc. (herein “SSL”) appeals the decision of the United States District Court for the Northern District of California, 1 granting summary judgment in favor of Lockheed Martin Corporation based on the court’s ruling of invalidity of SSL’s United States Patent No. 4,537,375. Because the district court misapplied the law of “on sale,” 35 U.S.C. § 102(b), we reverse the summary judgment and remand for further proceedings.

BACKGROUND

The '375 patent is directed to an attitude control system for maintaining the position and orientation of a satellite. A satellite in orbit may drift out of position due to influences such as gravitational effects of the sun and moon and pressure from the solar wind, generally called “disturbance transients.” To return the satellite to its correct orbit and orientation various on-board devices are employed, such as momentum/reaction wheels or thrusters, which are small rocket engines. Such corrective maneuvers are called “station keeping.” Imbalances in thruster power or misalignments with respect to the satellite’s center of mass, which may change as fuel is consumed, tend to introduce new errors in position or orientation during station keeping maneuvers. Such new errors require further correction after the primary correcting maneuver is made.

The novel method of station keeping described in the '375 patent is called the “prebias” technique. By this technique a correction for thruster imbalances is made before the primary station keeping maneuver is performed, using data stored from previous maneuvers. If any attitude inaccuracies remain they are subjected to a further correction, but as a result of the prebias step substantially less fuel is required overall than would be consumed without the prebias compensatory action. *1078 Conservation of on-board fuel prolongs the effective life of a satellite. Claim 1 of the '375 patent follows:

1. For use in a spacecraft during a change in velocity maneuver, the spacecraft employing a plurality of thrusters, at least a first thruster and a second thruster being disposed to develop mutually counteractive moment arms of thrust relative through at least one axis through a center of mass of the spacecraft, said first thruster and said second thruster being capable of developing unequal moment arms of force, a method of counteracting disturbance transients comprising the steps of:
storing prior to said maneuver a value representative of an estimated disturbance torque;
modulating in response to said stored value one of said first and second thrusters during said maneuver to counteract an actual disturbance torque a sufficient amount to compensate for said actual disturbance torque in order to minimize a net position error without initially detecting said net position error; thereafter
detecting said net position error, said net position error being indicative of a difference between said estimated disturbance torque and said actual disturbance torque with respect to said axis; and thereafter
modulating in response to a sum of said stored value and said net maneuver to counteract said actual disturbance torque to further minimize said net position error.

The district court held that the invention claimed in the '375 patent was on sale more than one year before the patent application was filed, rendering the patent invalid pursuant to § 102(b) (a patent is barred if the invention was “on sale in this country, more than one year prior to the date of the application for a patent in the United States”). Since the '375 application date is April 21, 1983, the “critical date” for the on sale bar is April 21, 1982.

The relevant events are not in dispute. Ford Aerospace and Communications Corp., a predecessor of SSL and the initial assignee of the '375 patent, entered into a contract with SociJtJ Nationale Industr-ielle Aerospatiale, a French company that had contracted with the Arab Satellite Communications Organization to develop the “Arabsat” satellite system. Ford was responsible for several aspects of the Ar-absat system, including the satellite attitude control system.

Dr. Fred Chan, a Ford employee, conceived of the prebias method of satellite station keeping as a potential improvement over the design that was originally intended to be used. On March 19, 1982 Ford sent Aerospatiale a document entitled “Engineering Change Proposal” (ECP) which described the prebiasing idea and how Dr. Chan proposed to achieve it, by the steps of storing an estimated disturbance torque, performing a first thruster modulation in response to the stored value, detecting the net position error, and then performing a second modulation in response to the net position error and the stored value. Included were Dr. Chan’s rough drawings, along with an estimate of the cost of developing the system. The district court held that this submission was an invalidating on sale event. Applying Pfaff v. Wells Electronics, Inc., 525 U.S. 55, 119 S.Ct. 304, 142 L.Ed.2d 261, 48 USPQ2d 1641 (1998), the court ruled that the ECP was a commercial offer of sale, and that the invention was ready for patenting because “SSL admitted] that Dr. Chan had legal conception of every element of every claim of the '375 patent at the time the ECP was submitted to Aerospatiale.” The court held that it was irrelevant that the inventor was *1079 uncertain whether the system could be made to work.

DISCUSSION

Summary judgment is appropriate when “there is no genuine issue as to any material fact and ... the moving party is entitled to a judgment as a matter of law.” Fed.R.Civ.P. 56(c). In this case there was no dispute as to what transpired; the issue was whether the criteria of the on sale bar were met. In Pfajf, supra, the Supreme Court held that the on sale bar arises when the invention is both (1) ready for patenting and (2) the subject of a commercial offer for sale. SSL states that neither of these criteria was met.

SSL states that at the time the engineering proposal was sent to Aerospatiale and for many months thereafter, Dr. Chan’s idea was not ready for patenting for its feasibility was not yet known and it had not been enabled. Dr. Chan testified that at the time he sent the proposal to Aerospatiale he had conceived of the idea but he did not know whether he could make it work. He testified that the method for generating a value had to be developed, and that he was not sure he could establish a stable control loop. He stated that it was not until many months later, after development and testing of an engineering model, that he determined that the idea would work.

Lockheed presented no evidence disputing Dr.

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271 F.3d 1076, 60 U.S.P.Q. 2d (BNA) 1861, 2001 U.S. App. LEXIS 24360, 2001 WL 1403311, Counsel Stack Legal Research, https://law.counselstack.com/opinion/space-systemsloral-inc-v-lockheed-martin-corporation-cafc-2001.