Definition: In this task you are given data in tabular format and a question. Write an **incorrect** ansswer to this question based on the information in the table.
Input: Table: ['Model name', 'Date', 'Type', 'Thrust (kg) / Power (eshp)', 'Fitted to']. ['RTD-1/VDR-2', '1938', 'Two-stage centrifugal compressor Turbojet', '500 kg estimated', 'Test-bed only']. ['S-18/VDR-3', '1945', 'Axial flow compressor Turbojet', '1,250 kg', 'Gu-VRD project']. ['TR-1', '1946', '8-stage Axial flow compressor Turbojet', '1,300 kg', 'Alekseyev I-21, Ilyushin Il-22, Sukhoi Su-10, Sukhoi Su-11']. ['TR-1A', '1947', '8-stage Axial flow compressor Turbojet', '1,500 kg', '']. ['TR-2', '1947', '', '', 'projected growth version of TR-1']. ['TR-3 and AL-5', '1949', '7-stage Axial-flow Turbojet', '4,600 kg (at qualification in 1950)', 'Il-30, Il-46, Lavochkin Aircraft 190, Tu-86, Yak-1000, Su-17(1949), Aircraft 150']. ['TR-7', '1950s', 'supersonic compressor prototype of the AL-7', '', 'Prototype for AL-7']. ['AL-7', '1954', '9-stage supersonic compressor Turbojet', '6,500 kg', 'Il-54, Su-7B, Tu-98, Su']. ['AL-21', '1961', '14-stage Axial compressor with variable stator blades', '11,000 kg', 'Yak-38, Tu-28/Tu-128, Su-17, Su-24']. ['AL-31', '1976', 'Twin-spool Turbofan 0.6 bypass ratio.', '13,300 kg', 'Su-27, Su-30, Su-34, Su-35, Su-47 Berkut']. Question:what are the thrust powers of the models?
Output:
2 strokes, 2 strokes, 2 strokes, 1 stroke, 8 strokes, 2 strokes, 2 strokes