Horwath v. Comm'r

2004 T.C. Memo. 213, 88 T.C.M. 279, 2004 Tax Ct. Memo LEXIS 219
CourtUnited States Tax Court
DecidedSeptember 21, 2004
DocketNo. 16927-02
StatusUnpublished

This text of 2004 T.C. Memo. 213 (Horwath v. Comm'r) is published on Counsel Stack Legal Research, covering United States Tax Court primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Horwath v. Comm'r, 2004 T.C. Memo. 213, 88 T.C.M. 279, 2004 Tax Ct. Memo LEXIS 219 (tax 2004).

Opinion

TIBOR GUENTHER HORWATH AND CHRISTEL HORWATH, Petitioners v. COMMISSIONER OF INTERNAL REVENUE, Respondent
Horwath v. Comm'r
No. 16927-02
United States Tax Court
T.C. Memo 2004-213; 2004 Tax Ct. Memo LEXIS 219; 88 T.C.M. (CCH) 279;
September 21, 2004, Filed

Commissioner's determinations of deficiencies and accuracy-related penalties sustained.

*219 Tibor Guenther Horwath and Christel Horwath, pro sese.
Dustin M. Starbuck, for respondent.
Chiechi, Carolyn P.

Chiechi

MEMORANDUM FINDINGS OF FACT AND OPINION

CHIECHI, Judge: Respondent determined the following deficiencies in, and accuracy-related penalties under section 6662(a) on, petitioners' Federal income tax (tax):

   Year    Deficiency    Accuracy-Related Penalty

   ____    __________    ________________________

   1997    $ 58,427.00       $ 7,157.80

   1998     45,435.00        6,824.40

The issues remaining for decision are:

(1) Are petitioners entitled for each of the taxable years at issue to the depreciation deduction that they claim? We hold that they are not.

(2) Are petitioners entitled for the taxable year 1998 to a deduction of $ 14,686 for travel expenses? We hold that they are not.

(3) Are petitioners liable for each of the taxable years at issue for the accuracy-related penalty under section 6662(a)1? We hold that they are.

*220 FINDINGS OF FACT

Most of the facts have been stipulated and are so found.

Petitioners resided in Falmouth, Virginia, at the time they filed the petition in this case.

In 1988, petitioners formed TG&C Associates, Inc. (TGC), an S corporation, that at all relevant times provided consulting services to various corporate and government entities. At all relevant times, TGC's principal place of business was located in petitioners' residence.

During the taxable years at issue, petitioners were the only two stockholders of TGC. For each of the taxable years at issue, each petitioner had a zero basis in the TGC stock that each owned.

During the taxable years at issue, petitioner Tibor Guenther Horwath (Mr. Horwath) occasionally provided consulting services as a sole proprietorship known as "Tibor G. Horwath, Consulting" (Tibor Horwath Consulting).

Claimed Depreciation Deductions

On June 24, 1992, TGC entered into contract DASG60-92-C-0069 (1992 contract) with the United States Army Strategic Defense Command (SDC). During the course of the 1992 contract, SDC paid TGC a total of $ 1,049,117.

The 1992 contract provided in pertinent part with respect to the specific tasks to be completed*221 pursuant to that contract:

   The following specific tasks will be performed under the

   proposed program:

   Phase I:

     (1) Design and construct an experimental SSPG [small

     spinning projectile guidance] seeker and associated

     laboratory setup for open loop performance evaluation of

     the concept against computer generated and recorded, single

     and multiple target and background images.

     (2) Evaluate the performance of the SSPG seeker for various

     target and background conditions, including the presence of

     detector noise.

     (3) Determine performance limits for the SSPG seeker in

     terms of minimum detectable line of sight motion to the

     target, and its ability to extract target feature

     information.

     (4) Conduct analysis to determine valid parameter ranges

     for follow-on simulation effort, and attempt to define

     projected hardware implementations.

     (5) Prepare an interim report of the findings and

 *222     recommendations.

   Phase II:

     (1) Adapt the open loop SSPG seeker laboratory experiment

     for interfacing with a 6-DOF flight dynamics computer code

     for a hardware in the loop simulation.

     (2) Design and construct a line of sight (LOS) processor to

     extract guidance information from the SSPG seeker output

     signals.

     (3) Modify and update the existing 6-DOF flight dynamics

     code to include rapid spin and nutation, and optimize the

     code for interface with the line of sight processor and

     other relevant laboratory hardware.

     (4) Assemble the hardware in the loop simulation model

     using the above components, debug and calibrate, and

     perform simulation runs against simulated single and

     multiple target and background images.

     (5) Transfer the hardware and software of the simulation

     effort to the KHILS facility, interface with the KHILS

     equipment and conduct simulation against typical strategic

*223      and theater missile defense scenarios.

     (6) Conduct a top level projectile design, defining a basic

     configuration, essential parameters like mass, moments,

     ballistic characteristics, and guidance and control, for

     various potential applications.

     (7) Prepare an interim report and material for a briefing

     to the Government.

   Phase III:

     (1) Conduct an analysis effort aimed at determining the

     optimum selection of field test conditions, scaling of

     parameters and target representations, and prepare a test

     plan.

     (2) Design and construct an experimental guided SSPG test

     vehicle and launcher to be used in field tests.

     (3) Repackage and miniaturize the laboratory SSPG seeker

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