A gas turbine engine is mounted on an aircraft which can attain a maximum altitude of $11 \mathrm{~km}$ from sea level. The combustor volume of this engine is decided based on conditions at

(A) sea level

(B) $8 \mathrm{~km}$ altitude

(C) $5.5 \mathrm{~km}$ altitude

(D) $11 \mathrm{~km}$ altitude

A gas turbine engine is mounted on an aircraft which can attain a maximum altitude of $11 \mathrm{~km}$ from sea level. The combustor volume of this engine is decided based on conditions at

(A) sea level

(B) $8 \mathrm{~km}$ altitude

(C) $5.5 \mathrm{~km}$ altitude

(D) $11 \mathrm{~km}$ altitude

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