The maximum height that a man can jump is a bit over 70cm for the very best athletes. This is because the only thing that matters is how high your centre of gravity rises. I will assume 80cm.
Work is force times distance. Weight is the force $W = gm_0 $ and when you jump a height $h$ under Earth gravity of 9.8m/s with a weight $m_0$, $E = hgm_0$ is the work that gravity did to bring you to a stop at your maximum height (all of the kinetic energy being converted to potential energy).
The work you performed to initiate the jump is also force times distance. It equals the gravitational potential energy at the top of the jump exactly. When jumping on an asteroid, the length of your legs and your strength we will assume don't change (a fabric-based space suit has a springiness in the legs, so this is an approximation). You perform an equal amount of work to what you did on Earth, namely $E = 0.8m \times 9.8 m/s^2 \times m_0$.
Escape velocity is given by (see Space Mission Engineering: The New SMAD edited by Wertz, Everett & Puschell, 2011, p. 201) $V_e = \sqrt{2GM/R}$ where $G = 6.674 \times 10^{-11}m^3 kg^{-1}s^{-2}$ is the gravitational constant, M the mass of the central body and R your distance from its centre (I assume for simplicity it is circular).
Density $\rho$ is in the region of $1000kg/m^3$ for icy bodies and $3000kg/m^3$ for rocky ones. In the case of a nickel-iron body we will approximate the overall density as $8000kg/m^3$.
We want to calculate the diameter R of a body where your kinetic energy at escape velocity equals $E$ above.
$$0.8m \times 9.8m/s \times m_0 = E = KE = 0.5m_0 \times V_e^2$$
$$0.8m \times 9.8m/s^2 = 0.5 \times V_e^2 $$
$$ 15.68 m^2/s^2 = V_e^2 = 2GM/R $$
still assuming a sphere
$$ M = \rho \times V = \rho \times 4/3 \pi R^3 $$
$$15.68 m^2/s^2 = 8/3 G \rho \pi R^2 $$
$$ \sqrt{(2.8 \times 10^{10} / \rho) m^{-1} kg } = R$$
Substituting the densities from above, we get roughly $R_{icy} \approx 5300m$, $R_{rocky} \approx 3100m$, $R_{iron} \approx 1900m$.
Now let's see what happens with your numbers. The astronaut can still do an equal amount of work to jump but their mass will be $m_1 = m_0 + m_{suit}$ on the asteroid, $\rho = 2000kg/m^3$. A NASA study from 1996 (see The Origins and Technology of the Advanced Extravehicular Space Suit by G.L. Harris, American Astronautical Society History Series Volume 24, 2001, p. 455) specified a maximum pressure suit assembly mass of 27kg for missions to Mars. This excludes the life support systems, for comparison Apollo had (see p. 440) 63.2kg of life support on a suit of 100kg total. We'll assume the future suit is a form-fitting elastic suit with almost all mass in life support, giving no springiness in the legs and massing just $m_{suit} = 30kg$ total. Note: You gave the astronaut weight as 30kg. This is a small child so I assume 70kg is intended instead.
$$ 0.8m \times 9.8m/s^2 \times m_0 = E = KE = 0.5 m_1 \times V_e^2 $$
$$ 0.8m \times 9.8m/s^2 \times 70kg = 0.5 \times 100kg \times V_e^2 $$
$$ 10.976 m^2/s^2 = V_e^2 = 2GM/R = 8/3 G \rho \pi R^2 = 8/3 \times 6.674 \times 10^{-11} m^3 kg^{-1} s^{-2} \times 2000 kg/m^3 \times \pi \times R^2$$
$$R^2 = 9.815 \times 10^6 m^2 $$
$$R \approx 3100 m $$
It only happens to be close to the rocky body approximation above because the increase in mass was made up by the decrease in gravity.
Edit: Finally, since you want mass:
$$ M = 4/3 \pi R^3 \times \rho = 4/3 \times 2000kg/m^3 \times \pi \times (3100m)^3 = 2.50 \times 10^{14} kg $$
Really finally this time: Since you updated the mass to 80kg and we may assume a suit mass of 10kg included in that, here's how the answer would change from my 100kg with 30kg suit mass answer:
$$V_e^2 = 10.976m^s/s^2 \times 100kg/80kg = 13.720m^2/s^2$$
$$R \approx 3100m \times \sqrt{100kg/80kg} \approx 3500m$$
$$M = 2.50 \times 10^{14}kg \times (\sqrt{100/80})^3 = 3.6 \times 10^{14}kg$$