Please read the following table in HTML format from a webpage and then answer the question in detail according to the table. Each table cell is defined by a <td> and a </td> tag. Each table row starts with a <tr> and ends with a </tr> tag. 'rowspan=m' and 'colspan=n' represents a cell spaning over 'm' rows and 'n' columns.

Webpage title:
Saturn V
Table title:
Soviet N1-L3
Table:
<table id='hittask' contenteditable='False'>
<tr> <th colspan=1 rowspan=1 >  </th><th colspan=1 rowspan=1 > Saturn V (Apollo 11) </th><th colspan=1 rowspan=1 > N1-L3 </th></tr>
<tr> <td colspan=1 rowspan=1 > Diameter, maximum </td><td class="highlighted"  colspan=1 rowspan=1 > 33 ft (10 m) </td><td colspan=1 rowspan=1 > 56 ft (17 m) </td></tr>
<tr> <td colspan=1 rowspan=1 > Height w/ payload </td><td class="highlighted"  colspan=1 rowspan=1 > 363 ft (111 m) </td><td colspan=1 rowspan=1 > 344 ft (105 m) </td></tr>
<tr> <td colspan=1 rowspan=1 > Gross weight </td><td colspan=1 rowspan=1 > 6,478,000 lb (2,938 t) </td><td colspan=1 rowspan=1 > 6,030,000 lb (2,735 t) </td></tr>
<tr> <td colspan=1 rowspan=1 > First stage </td><td colspan=1 rowspan=1 > S-IC </td><td colspan=1 rowspan=1 > Block A </td></tr>
<tr> <td colspan=1 rowspan=1 > Thrust, SL </td><td colspan=1 rowspan=1 > 7,500,000 lbf (33,000 kN) </td><td colspan=1 rowspan=1 > 10,200,000 lbf (45,400 kN) </td></tr>
<tr> <td colspan=1 rowspan=1 > Burn time, s </td><td colspan=1 rowspan=1 > 168 </td><td colspan=1 rowspan=1 > 125 </td></tr>
<tr> <td colspan=1 rowspan=1 > Second stage </td><td colspan=1 rowspan=1 > S-II </td><td colspan=1 rowspan=1 > Block B </td></tr>
<tr> <td colspan=1 rowspan=1 > Thrust, vac </td><td colspan=1 rowspan=1 > 1,155,800 lbf (5,141 kN) </td><td colspan=1 rowspan=1 > 3,160,000 lbf (14,040 kN) </td></tr>
<tr> <td colspan=1 rowspan=1 > Burn time, s </td><td colspan=1 rowspan=1 > 384 </td><td colspan=1 rowspan=1 > 120 </td></tr>
<tr> <td colspan=1 rowspan=1 > Orbital insertion stage </td><td colspan=1 rowspan=1 > S-IVB (burn 1) </td><td colspan=1 rowspan=1 > Block V </td></tr>
<tr> <td colspan=1 rowspan=1 > Thrust, vac </td><td colspan=1 rowspan=1 > 202,600 lbf (901 kN) </td><td colspan=1 rowspan=1 > 360,000 lbf (1,610 kN) </td></tr>
<tr> <td colspan=1 rowspan=1 > Burn time, s </td><td colspan=1 rowspan=1 > 147 </td><td colspan=1 rowspan=1 > 370 </td></tr>
<tr> <td colspan=1 rowspan=1 > Total impulse </td><td colspan=1 rowspan=1 > 1.7336×109 lbf (7.711×106 kN)·s </td><td colspan=1 rowspan=1 > 1.789×109 lbf (7.956×106 kN)·s </td></tr>
<tr> <td colspan=1 rowspan=1 > Orbital payload </td><td colspan=1 rowspan=1 > 264,900 lb (120.2 t) </td><td colspan=1 rowspan=1 > 209,000 lb (95 t) </td></tr>
<tr> <td colspan=1 rowspan=1 > Injection velocity </td><td colspan=1 rowspan=1 > 25,568 ft/s (7,793 m/s) </td><td colspan=1 rowspan=1 > 25,570 ft/s (7,793 m/s) </td></tr>
<tr> <td colspan=1 rowspan=1 > Payload momentum </td><td colspan=1 rowspan=1 > 2.105×108 slug-ft/s (9.363×108 kg·m/s) </td><td colspan=1 rowspan=1 > 1.6644×108 slug-ft/s (7.403×108 kg·m/s) </td></tr>
<tr> <td colspan=1 rowspan=1 > Propulsive efficiency </td><td colspan=1 rowspan=1 > 12.14% </td><td colspan=1 rowspan=1 > 9.31% </td></tr>
<tr> <td colspan=1 rowspan=1 > Earth departure stage </td><td colspan=1 rowspan=1 > S-IVB (burn 2) </td><td colspan=1 rowspan=1 > Block G </td></tr>
<tr> <td colspan=1 rowspan=1 > Thrust, vac </td><td colspan=1 rowspan=1 > 201,100 lbf (895 kN) </td><td colspan=1 rowspan=1 > 100,000 lbf (446 kN) </td></tr>
<tr> <td colspan=1 rowspan=1 > Burn time, s </td><td colspan=1 rowspan=1 > 347 </td><td colspan=1 rowspan=1 > 443 </td></tr>
<tr> <td colspan=1 rowspan=1 > Total impulse </td><td colspan=1 rowspan=1 > 1.8034×109 lbf (8.022×106 kN)·s </td><td colspan=1 rowspan=1 > 1.833×109 lbf (8.153×106 kN)·s </td></tr>
<tr> <td colspan=1 rowspan=1 > Translunar payload </td><td colspan=1 rowspan=1 > 100,740 lb (45.69 t) </td><td colspan=1 rowspan=1 > 52,000 lb (23.5 t) </td></tr>
<tr> <td colspan=1 rowspan=1 > Injection velocity </td><td colspan=1 rowspan=1 > 35,545 ft/s (10,834 m/s) </td><td colspan=1 rowspan=1 > 35,540 ft/s (10,834 m/s) </td></tr>
<tr> <td colspan=1 rowspan=1 > Payload momentum </td><td colspan=1 rowspan=1 > 1.1129×108 slug-ft/s (4.95×108 kg·m/s) </td><td colspan=1 rowspan=1 > 5.724×107 slug-ft/s (2.546×108 kg·m/s) </td></tr>
<tr> <td colspan=1 rowspan=1 > Propulsive efficiency </td><td colspan=1 rowspan=1 > 6.17% </td><td colspan=1 rowspan=1 > 3.12% </td></tr>
</table>
Question:
How big was the Apollo spacecraft?
Answer:
The Apollo spacecraft is 363 feet (111 m) tall and 33 feet (10 m) in diameter.